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Apollo 15

Day 4: Lunar Orbit

Corrected Transcript and Commentary Copyright © 1999-2008 by W. David Woods and Frank O'Brien. All rights reserved.

[Flight Plan page 3-084.]

[As the crew begin their first meal in lunar orbit, the S-band auxiliary channel, which can be set to transmit science data from the SIM (Scientific Instrument Module) bay or TV from the onboard TV camera, is switched to Science. The Gamma-ray Spectrometer and the Alpha Particle experiment are switched on to begin the sequence of orbital science. Both of these instruments can collect data from the Moon from either the day or night sides. Other instruments, such as the cameras and the X-ray Spectrometer rely on sunlight to work.]

[Mission Control have been replaying the DSE (Data Storage Equipment), an onboard tape recorder for storing digital data and cabin voice. It had been recording telemetry from the spacecraft, including the big engine, while the LOI (Lunar Orbit Insertion) burn was taking place over the far side of the Moon. With communications with Earth restored, Mission Control can replay the tape and see how the systems have performed.]

079:13:35 Scott: Houston, 15.

079:13:37 Henize: We've just got through with the [DSE] playback, and we've got excellent burn data down here. And, if you'll give us Accept we'll send up a REFSMMAT.

079:13:47 Scott: Okay; you've got P00 and Accept.

079:13:52 Henize: Thank you.

[By asking the crew to select Program 00 (POO in the shorthand of Apollo) and the Accept mode on the computer, Mission Control are able to uplink data directly into it. In this case, they are sending up a new REFSMMAT.]

[Apollo 15's guidance platform is currently aligned to the LOI REFSMMAT, matching the orientation of the spacecraft during the LOI burn. Soon, Al will change it to the landing site REFSMMAT which is just now being uplinked to the spacecraft. This new orientation is defined as the orientation of the landing site, with respect to the stars, at the time of landing; and is chosen so that the FDAI or "8-ball" in the LM will display 0° in all three axes at the ideal time and place of landing, assuming it lands in a fully upright attitude. Note that this ideal landing attitude is never achieved in real landings because of the relentlessly undulating nature of the lunar surface.]

[To change to this new platform alignment, Al will carry out the P52 realignment process twice; once to the LOI REFSMMAT, so that the drift of the platform since the last P52 can be measured and eliminated, and again to swing it around to the

landing site REFSMMAT.]

079:14:49 Henize: Excellent. If I'm not mistaken, this is probably the first time men have been over Crisium.

079:14:59 Scott: I guess that's probably right.

[As seen from Earth, the landing site is 26° north of the centre of the lunar disk and Apollo 15 has entered an inclined orbit to take it over the site. As previous missions had landing sites located near the lunar equator, none had orbited at such an inclination. Having reappeared around the eastern limb, and travelling roughly WNW, the crew are flying over new territory and have a close up view of Mare Crisium, a small but distinctive and isolated mare which is easily visible from Earth by the naked eye as a dark blotch, well to the right of the Moon as seen from the northern hemisphere. None ever reached the 11° to 24° latitude required to fly over Mare Crisium.]

[The Sun is high in the sky at Mare Crisium (Sea of Crises) and there are virtually no shadows to indicate relief. Variations in the landscape's reflectivity, or albedo, provide the dominant cues and betray the intrinsic hue of the various basalts and overlaying ejecta rays that come in from nearby impacts. Within the darker colour of the mare, fresh impact craters appear white from the intense shock sustained by the rocks, whose structure is riddled with countless tiny fractures which reflect and scatter sunlight.]

079:15:37 Scott: Another interesting fact that - that we've all noticed is that it - it looks like a great desert across which we've had a number of dust storms. And, in many places, you can see the - the tracks or the swirls across the surface which looks like a - a great dust storm has been blowing across the surface - primarily indicated by the albedo change. But all over Crisium, you can see the streaks, which obviously are from impact at some point or another, but the impression we get is that the [swirls are the] result of a dust storm.

079:16:12 Henize: Very interesting; 15. The computer's yours.

079:16:27 Scott: Say again.

079:16:29 Henize: The computer's yours.

079:16:32 Scott: Okay. [Long pause.]

[Now that Mission Control have uplinked the new REFSMMAT, the crew can place the Up Telemetry switch, next to the DSKY (Display and Keyboard), to Block (meaning to inhibit the passage of data) and begin using the computer again. This new orientation, one which is based on the orientation of the landing site, will be relevant until near the time the LM returns from the surface and will be first brought into play when the IMU platform is realigned in just over half an hour's time.]

[Isolated in the western half of Mare Crisium, Peirce, an 18.5 km diameter crater, is named after an American mathematician and astronomer and it provides a good initial example of one of the most powerful methods of understanding the history of the Moon - its stratigraphy. By observing which lunar features obscure which, a relative timeline of lunar history can be deduced. Subsequently, when the age of rocks from a particular feature is measured, part of the stratigraphic timeline can be tied to an absolute date, helping to narrow the range of possibilities for features related to it.]

[Mare Crisium is one of the simplest mare type formations on the Moon. It was formed when lava welled up from the Moon's interior to fill a primordial basin that had been carved out of the crust by the impact of a large meteoroid hundreds of millions of years previously. Sometime after the lava solidified, another smaller impact formed the crater Peirce as we can see today by its shape with respect to the mare. In August, 1976, the Soviet probe, Luna 24, landed on Mare Crisium, extracted a 1.6 metre core and returned it to Earth. From this sample, we know that the lavas which form this mare cooled 3.3 billion years ago and can deduce that the impact event which formed the Crisium basin occurred before this, while Peirce must have been blasted into the mare after this date.]

[Note that just because a crater exists within a mare, it does not necessarily mean that it is younger than the surrounding basalt. Some craters, Archimedes in Mare Imbrium is an example, predate the lavas which flowed up to and around their rims.]

Public Affairs Officer - "That was Al Worden."

079:17:39 Scott: And, you know, as we look at all this after the many months we've been studying the Moon, and learning all the technical features and names and everything, why - when you get it all at once, it's just absolutely overwhelming. There are so many different things down there, and such a great variety of land forms and stratigraphy and albedo, that's it's hard for the mental computer to sort it all out and give it back to you. I hope over the next few days we can sort of get our minds organized and get a little more precise on what we're seeing. But I'll tell you; this is absolutely mind-boggling up here.

079:18:15 Henize: Gentlemen, I can well imagine that a foreign planet must be a weird thing to see.

Public Affairs Officer - "That was Dave Scott."

079:18:25 Scott: And we've got Proclus in view right now.

[Proclus, named after an Athenian philosopher and mathematician, 410 - 485 A.D., is a 28 km diameter rayed crater beyond the western shore of Mare Crisium.

This is an Earth-based view of Proclus. Its rim is polygonal rather than circular and its remarkable ray system displays a 120° excluded zone to the west bounded by two prominent rays. A notch in the crater's rim at the apex of the excluded zone is opposed by another dominant ray sweeping across Mare Crisium. The cause of this striking layout and symmetry is believed to be due to the impactor striking at a distinct angle to the surface. However, at the time of Apollo 15, this theory had not been adopted. Al is scheduled to observe Proclus as part of his visual observation program during his solo flight in the CSM at 128 hours GET. In the light of his observations, a temporary theory is developed suggesting the exclusion zone is due to the effects of the surrounding landforms and geological faulting on the pattern of material ejection by the impact.]

079:18:37 Scott: Well, the - the rays extending from Proclus are very light in color for about - they are very light color for about - oh, 240 to 260 degrees around, and then there's a region of dark mare or albedo. And our - our orientation presently with the spacecraft is such that we have - we're having a tough time figuring out north and south; and, once we get on an orbit track, we'll be able to give you direction a little bit better. But the inner walls of Proclus are very light in color, almost white. The outer walls - the outer ring has a somewhat light gray appearance and the difference in the - the rays is really between a light and a dark gray as distinguished from the inner walls which are quite white. The - the walls exhibit some debris on the upper slopes, maybe the upper 30 percent. I can see, on one side of the - the crater, some large blocks. On another side, I can see what appears to be a large slump block or a large slumping of the wall that goes about halfway down and takes about - oh, 15 degrees of the rim of the crater with it. The floor is very irregular and rough, almost a constant gray - medium gray color, somewhat darker than the light gray on the outside rays and somewhat lighter than the dark gray on the - the surface, which does not seem to be covered with a ray pattern. There are a few ridges on the floor, arcuous ridges, and some domes which are quite prominent. And I'm sure when Al comes back over here later on and has a chance to study it carefully, he can give you a - a good accurate picture.

079:20:55 Henize: Beautiful.

[Long comm break.]

[The crew are due to use Program 20 to maneuver the spacecraft to an attitude which will permit photography of the lunar surface.]

[P20 accepts values from the crew to allow the computer to keep one side of the spacecraft facing a particular direction or object, in this case the centre of the Moon. Three of these values (Noun 78) represent the attitude the spacecraft is to hold, relative to whatever it is tracking. A fourth value (Noun 79) defines the accuracy to which the required attitude should be held (described as the deadband, the range of attitudes from the ideal for which there will be no corrective thruster activity). ±5° is punched in for this. Finally, the object to be tracked is defined in Noun 70 by entering its octal "starcode". Not all the objects which have starcodes are stars, as the Earth and Moon are also in this list with numbers 47 and 50 respectively. Since they wish the spacecraft to track the Moon, they enter 50 into Noun 70.]

[With all the values entered, the computer begins flashing "50" in the Verb display and "18" in the Noun display of the DSKY which essentially asks the crew if they would like to perform the auto-maneuver to the requested attitude. When the "Proceed" button is pressed, the computer fires the appropriate thrusters, causing the spacecraft to point the windows at the lunar surface and allowing photographs to be taken. The photography is not scheduled to begin until the beginning of the second revolution, midway around the far-side. The spacecraft will be crossing the terminator around this time where the low Sun angle will enhance the topography of the surface.]

079:21:51 Scott: Okay; very good. I wish we were in a...

079:21:54 Henize: Right. It's [in] 2 minutes, 40 seconds, but it's going to be out of your visual range, somewhere around the center area of the Moon.

079:22:07 Scott: Roger. It's too bad we won't get to see it. We'd already taken a look at the map to see if we'd have a chance, but I guess we'll miss that one. [Long pause.]

[Woods - "To what extent did your preparation in looking at photographs and looking at maps help you when you got into lunar orbit and looking out the window. Did you find it very easy to find your way about. Know what you're looking at."]

[Scott - "Yeah. Pretty much. You know where your orbit is. You've studied the features below your orbit. It's pretty familiar. Yeah. Comfortable kind of feeling because you know pretty much what's there."]

[Woods - "All the way across from one side to the other?"]

[Scott - "Yeah. We studied, you know, the general, larger features. Al, of course, knew a lot more detail."]

[Although photography is not scheduled for another hour and twenty minutes, a crew member has begun taking pictures of the landscape below using the Hasselblad camera, a 250-mm lens and film magazine M.]

[Between Mare Crisium and Mare Serenitatis (Sea of Serenity) lies a large, heavily battered region which is currently north of the spacecraft's position. AS15-91-12351 to 12360 show various landmarks in this area. Newcomb, named after Simon Newcomb, 1835 - 1909, an American astronomer, is well shown in

AS15-91-12353 with its sharply defined 39 km wall and a highly irregular outline, perhaps reflecting pre-existing faults in the terrain. Krichoff, seen at the bottom of 12357, is a distinct but highly eroded 25 km crater which carries the name of the German physicist, 1824 - 1887, who is well known for his work on spectroscopic analysis. 12360 dimly show a system of graben rilles, dropped floor valleys caused by extensional forces, which lead to the fractured pair of craters, Chacornac and Posidonius at the eastern shore of Mare Serenitatis. These rilles are arcuate, lying roughly parallel to the rim of the Serenitatis basin. As the Sun is high in the sky over these areas, there is little relief shown in these photographs.]

[The NASA PAO people are showing the news media the Apollo 14 seismometer chart in readiness for the impact of Apollo 15's S-IVB booster stage.]

[Apollo 15's current elliptical orbit has its low point over the Moon's far-side. Therefore, as they come towards their 315-km high point, or apocynthion, they can view across the entire width of Mare Serenitatis in one eyeful. Below them are the Montes Taurus which form the eastern rim of the Serenitatis basin while looking to the west, they can see Montes Haemus, the southwest range, and Montes Caucasus, the northwest range.]

[As they come up to the eastern shore of Mare Serenitatis, they take photographs AS15-91-12361 to 12364, looking north towards Chacornac, and the southern rim of Posidonius. In

12363, one of the graben rilles can be seen to cross the left wall of the degraded, Chacornac. The southern wall of Posidonius is to the right of this image. These two craters are like a matched pair in that they both have flat interiors, various rilles etch their surfaces, and they each sport a small, fresher, bowl-shaped crater slightly west of their centres. However, Posidonius, at 95 km diameter, has much more prominent walls than the disintegrated rim of 51-km diameter Chacornac and displays both of the major types of rille, the graben or dropped-floor rille and the sinuous rille, believed to have been formed by running lava. Posidonius, 135 - 51 B.C.E., was a Greek intellectual and Jean Chacornac, 1823 - 1873, was a French astronomer.]

[

AS15-91-12365 shows a triplet of craters to the north of Posidonius extending north into Lacus Somniorum. Beyond them is Daniell, an oval crater, 30 by 23 km, named for John Frederick Daniell, 1790 - 1843, the English inventor of the hygrometer.]

[

AS15-91-12366 to 12370 are a sequence that allows the spacecraft's motion to move the point of view westward, starting at the western rim of Posidonius and moving out into Mare Serenitatis. The final pair show the Gamma Prominence at the north end of Dorsa Smirnov, part of the complex of wrinkle ridges which snake over the mare. In 12370, a small, fresh crater with a light halo of ejecta around it punches the centre of the ridge. Dorsa Smirnov is, perhaps, the most prominent ridge on Mare Serenitatis. It is named after Sergei Smirnov, 1895 - 1947, a naturalist from the then Soviet Union.]

[As the spacecraft nears the terminator, the shadows are becoming longer and the subtle relief of the mare is now distinct.]

079:23:46 Worden: Okay, Karl. We're coming up over Serenitatis now. We're almost over le Monnier and we can see the Littrow area just out in front of us. And it is, in fact, about three different shades. You can see - in the upland area, and particularly what looks like down in the valleys, a darker color, and it does look like it's a light powdering - or dusting-over of the entire area. And then, as you get out further into Mare Serenitatis, there's another layering which is a little bit lighter in color. And then, out at the last edge of the wrinkle ridge, out beyond that is the last layer, and the rest of Serenitatis looks fairly - fairly light in color. So I'd say that the - the - centeral - central part of Serenitatis is light, out beyond the first wrinkle ridge is a darker layering, and we're not up close enough to see what it is yet, and then as you get up into the highlands around le Monnier and Littrow area itself, there's what - what appears to be a - a light dusting of dark material, and it certainly looks volcanic from here. Off to - to the left of that, to the south, we can pick up Sulpicius Gallus pretty clearly right now.

[Mare Serenitatis is visible from Earth as one of the eyes of the Man in the Moon - the right eye as we see it. The basalt which forms its surface is slightly darker in patches towards the shoreline, particularly in the east and southwest. This "dark mantling" was of considerable interest to the geologists involved in deciding where Apollo missions should land as they believed that it may be an indication of dark, volcanic material being spread over a older, slightly lighter surface. In effect, Al's training has cued him up to interpret the dark mantling as the result of relatively recent volcanism. It will take a proper study of the region by the crew of Apollo 17 to change the interpretation of the dark mantling. Prior to the Apollo 13 abort, and the subsequent decision to send Apollo 14 to its predecessor's landing site at Fra Mauro, NASA were planning to send 14 to some wrinkle ridges within the dark mantling near the eastern shore of Serenitatis.]

[Le Monnier, named after an 18th century French astronomer, is a 61-km crater flooded with the lavas from the mare to form a bay on its eastern shore. The area to the south is part of Montes Taurus and includes the 31-km crater Littrow with its flat floor and degraded rim. Johann von Littrow, 1781 - 1840, was an Austrian astronomer. Close by lies a valley which would become the landing site for Apollo 17 in seventeen months time, due in part to Al Worden's up-coming observations from orbit and the geologists desire to find evidence of lunar volcanism. See also

122:18:17 and, especially 128:12:46.]

[

AS15-91-12371 looks towards the southwest corner of Mare Serenitatis and the terminator between the lunar day and night. The illuminated rim of Sulpicius Gallus is visible lying in front of the lit peaks of Montes Haemus.]

[At 079:24:42, while Worden was describing the landscape in and around Mare Serenitatis, the S-IVB stage impacted the Moon at 1.0° S, 11.87°W, directly between the craters Sömmering and Turner, 188 km northeast of the Apollo 14 landing site and 355 km northeast of the Apollo 12 landing site.]

079:25:18 Worden: Well, after - after the King's training, it's almost like I've been here before.

[The person Al is referring to as "the King" is Farouk El-Baz, an important member of a team from Bellcomm that extensively studied the Moon's landforms with a view to landing site selection and which prepared the crews, especially Al, for their role as visual observers of the lunar surface. It is believed that Al is using this as a specific nickname for Farouk, rather than using it as an idiom of the period meaning "the best".]

[Scott, from 1998 correspondence - "I believe it was unique to Farouk as an individual, and not a generic term used by Al - it could have been related to Farouk's [Egyptian] origin; but it probably also had to do with their very close relationship, and perhaps some event that occurred during training."]

[Journal contributor Brian Lawrence adds "King Farouk I was king of Egypt from 1937 to 1952, when he was deposed in a coup by General Neguib. He was exiled in Italy from 1952-59 when he became a resident of Monaco. In exile he was a flamboyant, larger-than-life figure, with an extravagant playboy image and lifestyle. Since he was so well known, anyone named Farouk, who also happened to be Egyptian was bound to be called 'the King'."]

[Worden, from 1998 correspondence - "[Brian is] absolutely right about why we called Farouk 'The King'. In fact I guess I probably started it. I don't know if you are aware of his history, but he defected from Egypt because they would not recognize his marriage to Pat, a wonderful Boston Irish red head. So, Farouk left the country, came to the US, where he had gone to college, and eventually joined the team that helped us with training. Now he is a distinguished visitor, consultant, lecturer and tour guide for the Egyptian government. Strange how things can turn around, given enough time."]

[Bellcomm was a subsidiary of the huge AT&T telephone and communications company. Formed to meet NASA's needs in analysing many aspects of the Apollo program in 1962, it merged with Bell Laboratories ten years later, its involvement with Apollo completed.]

[Scott - "Another thing NASA did right in those days was to form Bellcomm. Bellcomm was superior, excellent, really good people. And they had the werewithall and the capability to go sit in any mission, any time and report to headquarters - report - tell headquarters what they're learning and advise headquarters on certain things."]

[Woods - " Was part of the value of that, that they were not of NASA. That they could stand back and see a bigger picture."]

[Scott - "Yeah. Definitely. They were independent. Bob Seamans formed that early on to get an independent headquarters assessment of what was going on and evaluation. And, you know, Bellcomm is one of the few government agencies that, after it completed its mission, dissolved itself and went away. When Apollo was over, it went away. Pretty good."]

[O'Brien - "Why was Bellcomm deemed as a necessary thing? Why wasn't that kind of function brought into the MSC at the time?"]

[Scott - "In the very early stages, the talent wasn't around to go to the Moon. So Webb and Seamans, as I recall, thought, 'We should go hire some outside talent that advises us. We're the managers. We have to make decisions. We need some very good people from the outside to watch how our people make decisions, and see if we're going in the right direction. So we'll go hire some people.' They started out with just a few. Went to Bell Labs and then it built up to whatever it built up to. You know, checks and balances. Reporting to the boss. It's always good. Bellcomm didn't have any real authority, but they went to the boss at headquarters and said we recommend this or suggest that or whatever. And it gave the bosses an independent assessment."]

[Woods - "Did they actually take part in the planning process?"]

[Scott - "Oh yeah, they did. They were heavily involved, as I recall, in MPAD [Mission Planning and Analysis Division] because they looked at other kinds of things. But they didn't get within, other than attending meetings and writing memos, they were not in the chain of command. They were not in the management process at that level."]

[Woods - "They also seemed to be heavily involved in landing site selection. Was that to try and cut through the NASA bureaucracy of trying to find one?"]

[Scott - "Expert advice. That's why they were hired; as experts, so expert advice. And they did a lot on 15 too. In fact, Jim Head wrote a great memo on Hadley. The reasons for and attributes for, because he was a geologist, an expert geologist. NASA had expert geologists too but not at that level."]

[The seismic waves from the S-IVB impact reach the Apollo 14 seismometer at 079:25:19, 37 seconds after the event. Their speed through the lunar crust is therefore 5.08 km/second.]

079:25:28 Scott: And, Karl. We're approaching the Apennine Mountains, and that is indeed a spectacular view.

079:25:34 Henize: Roger...

079:25:35 Worden: Sure is, Karl. No question about those mountains being there and where we're at with them.

[Apollo 12's seismometer is now reacting to the S-IVB impact, which it first picks up at 079:25:38, 55 seconds after the event. This time, the seismic tremors have travelled at the greater speed of 6.45 km/sec.]

079:25:52 Worden: Yes; tremendous relief as we approach the mountain, Karl.

[Two photographs, AS15-91-12372 and 12373, look north at the western shore of Mare Serenitatis, where the mare lavas form numerous embayments with the foothills of Montes Caucasus. The lighting is very oblique in this pair of images as, just beyond the peaks on the western side of the image, Mare Imbrium (Sea of Rains) is still in lunar night. They are about to pass over the landing site at Hadley, 300 km below them, but will not see it as it is also in darkness in a bay shadowed by the Montes Apenninus, a mountain chain which runs continuous from the southern end of the Caucasus chain and which forms the southeastern rim of the Imbrium basin.]

[When discussing lunar geology, it is important to make a distinction between the mare, which are the large areas of basalt responsible for the dark markings over the lunar surface, and the basins, which often provide the supporting structure for the layers of mare basalt. Viewed in this light, the Apennine mountains are an exposed part of the rim of the Imbrium Basin, a huge impact-formed structure. Mare Imbruim consists of the layers of basalt solidified from vast quantities of lava that poured out from the Moon's interior to fill the Imbrium Basin. Half a billion years separates the formation of the basin in a catastrophic event 3.84 billion years ago and its subsequent filling with mare basalts.]

079:26:50 Henize: 15, this is Houston. There is no update required on your T - on your TEI-4 PAD.

[The TEI-4 PAD was read up to the crew at 076:42:48. Mission Control are happy that it is still valid even after the LOI burn,]

[In 1651, Giovanni Riccioli drew up a map of the Moon which established much of the lunar nomenclature we see today and, mistakenly, used the word "mare" for the prominent dark markings, invoking the metaphor of the sea. Yet despite Riccioli's "mistake", Dave is driven to invoke the maritime analogy again to describe Mare Serenitatis' similarity to a great ocean lapping at the mountains around its edge.]

079:27:48 Scott: Rog, but I'm afraid it'll be dark today.

079:27:51 Henize: That's right.

[When Falcon lands in the lunar morning, the Sun will have risen 12° above the local horizon. There is still a day to go before the landing and in that time, the Sun will move through 12° of lunar sky. Therefore, if the Moon were a smooth sphere, the Sun would just now be rising over Hadley. However, the site is shadowed by the Apennines and the crew will not get a chance to look at it until after their rest period.]

[The 12° Sun angle is much steeper than the 5° of previous missions. However, Apollo 15 is the first flight to approach the landing site at a 25° approach angle (12 to 14° had been used previously) to give the LM clearance over the peaks to the east of Hadley. The rule of thumb used by mission planners is that the elevation of the Sun behind the LM should be roughly half the approach angle to make the shadows of any craters and boulders visible to the crew. Yet, if the launch from Earth had been delayed by a day or so, the planners deemed that up to 24° would be acceptable.]

[The 12.2-km crater, Sulpicius Gallus, lies near the south western edge of Mare Serenitatis in another in-shore area which displays dark mantling and, like the Littrow area, had been thought to be possibly volcanic. Al is continuing with this interpretation, based on his tutoring from Farouk El-Baz. Sulpicius Gallus was named after a Roman consul and scholar (c. 168 B.C.E.) who is honoured for predicting a lunar eclipse on the eve of a battle at Pydna, Macedonia.]

079:29:00 Scott: And Houston; we're coming up here on the terminator and the area, I guess we call Crackled Hills really looks like crackled hills. If you distinguish between the mountains, which are very prominent and smooth, the surface between the first small mountain range and the - what is now the terminator, is relatively flat with a very rough texture - very irregular, lower, crackled hills.

[Dave appears to be describing the "intra-massif." The true mountains are huge faulted blocks or massifs which form the highest summits along the rim of the Imbrium impact basin and which Dave describes as prominent and smooth. Further out from the centre of the basin, beyond the massifs, is the hummocky intra-massif which Dave is calling the "Crackled Hills" and which is nowadays known as the Alpes Formation. This is believed to be material from the impact event which formed the basin and which was deposited moments later just outside the rim, not having enough energy to travel further. Experiments with artificial impacts under laboratory conditions suggested that this may be the deepest material excavated by the impact, though lunar geologists are less certain of this nowadays and are unsure of its origin.]

[Woods, from 1998 correspondence with Scott - "Can you remember what area of lunar surface you were referring to as the Crackled Hills? Was it an unofficial name among yourselves and the geologists on the ground?"]

[Scott, from 1998 correspondence - "It probably was an unofficial name based on preflight discussions. As you are probably aware, prior to the mission, we covered many, many topics, areas, concepts, hypotheses, and other forms of geological discussions with the most prolific professors and teachers who existed at the time. And many (most) of these discussions, especially those after dinner in the crew quarters, were great fun, as well as the source of names, anecdotes, and other 'inside information' among the team who were preparing us for this unique expedition. During our planning (and learning) of lunar orbit, the amount of time even Jim and I would have in lunar orbit was remarkable, especially at the high inclination and over new 'ground.' Thus we had many, many 'inside' comments to make as we cruised along the lunar trails (tracks)!"]

079:29:47 Scott: Jim calls it a gun-metal gray, and that's a very good term, I think, for the color that we're seeing now. And as we approach the terminator, of course, the relief stands out even more. The shadows are getting much longer, and the peaks of the mountains, as they're silhouetted against the - the Crackled Hills, seem to have a - a diffuse shadow at the top. The shadow, as it goes from the base of the mountain to it's peak, is very sharp. And around the top of the mountain, it becomes more diffuse, not - not quite as sharp and begins to blend in with the - the surface on which it's being cast.

[Dave's description of the change in the nature of the shadow implies that the mountains he is looking down upon have very rounded summits. Before the era of spaceflight, many artists, even those informed by astronomy, had depicted the Moon's topography to be very rough and craggy, almost jagged. They had not reckoned with the great antiquity of the lunar surface and the slow, relentless wearing-down of the rocks by aeons of bombardment from space by the constant rain of micrometeorites. David Harland, author of Exploring the Moon: The Apollo Expeditions and who reviewed this journal, points out how remarkably clear the mountains are of craters.]

[Journal contributor David Harland - "The mountains are blocks of crust that were thrust up through the overburden of rubble from all of the earlier impacts (in the case of the Apennines, the Imbrium impactor shoved blocks up through ejecta from the earlier Serenitatis forming event), and much of this overburden slumped down off the block to form a thick talus in the 'valleys' between. The slopes of the massifs are so thick with this talus that slumping tends to erode away craters (meteorites are just as likely to hit a hill as a plain) rapidly, at least compared to a crater out on the plain. There is, therefore, very little 'rough terrain' on a mountain slope, and this helps create the impression of smoothness. Another point is that impacts preferentially toss stuff downslope, so a process of 'mass-wastage' tends to clear the summit of thick overburden and, as Apollo 15 found, there is knobby terrain on top, where the outcrops show through. Compared to the scale of the peak though, this relief is fine detail."]

[Comm break.]

[The southeastern shore of Mare Imbrium is conventionally thought to be bordered by the great arc of Montes Apenninus, huge mountain-sized, up-thrusted blocks which are remnants of the landscape's near-instantaneous alteration by the asteroid impact that created the Imbrium basin. The landscape of this area is, however, complicated by a number of formations. After the basin was formed, flows of light-coloured lavas created the Apennine Bench Formation, a light patch seen to extend from the centre of the Apennine Front halfway to the centre of Mare Imbrium.

The Apennine Bench Formation is visible from Earth with the naked eye. Photo courtesy of Rob Gendler. A large meteor struck this patch, leaving the 83-km crater Archimedes and covering the Bench with ejecta. When the mare-filling epoch began on the Moon, the lavas which formed Mare Imbrium also flooded Archimedes but did not inundate the Bench. Subsequently, two more strikes added the craters Aristillus and Autolycus, like Archimedes, named after prominent figures from Greek science and making up the distinctive trio of craters we see today. These two younger members of the trio display well formed ejecta blankets over the mare surface which show they were formed after the mare. Dave is describing this barely lit ejecta blanket which appears particularly rough in the very early morning light. Autolycus is the smallest at 39 km while the 55-km Aristillus displays a triple central peak.]

[Separate to the lava flows of Mare Imbrium, an outpouring of lava deposited mare basalt across the Apennine Bench Formation between the Apennine Front and Archimedes from a vent named Bela within the Apennine Front, 60 km southwest of the landing site. This dark area is called Palus Putredinus (March of Decay). The lava flowed along a sinuous channel which remains as Hadley Rille and which snakes roughly parallel to the Apennine Front and slightly offshore, leaving a strip of mare between the rille and the mountains. Falcon will land within an embayment in the Apennine's convoluted shoreline along this strip, flanked by two major mountains; Hadley to the northeast and Hadley Delta to the southwest. Hadley C is a small crater on the mare on the opposite side of Hadley Rille and 30 km southwest of the landing site. The features in this area were named after John Hadley, 1682-1743, an Englishman who pioneered optical instruments, especially the development of the reflecting telescope.]

079:33:31 Scott: Yes that's true. Aristillus and Autolycus both have their eastern rims exposed to the sunlight and we get a pretty good look at the elevation on the rim. And Autolycus, to it's north eastern side, seems to have a - a saddle or somewhat depressed rim. And as you come around to the west - the eastern side of Aristillus, it seems to be relatively level or horizontal, with a few subtle saddles and depressions. Autolycus appears to have a - a relatively horizontal or - or even rim all the way around, and we can see sunlight on the northwestern side of Autolycus, on the rim, just barely a tick of it.

079:34:28 Henize: Roger. It sounds like a fantastic view.

079:34:35 Worden: It really is.

079:34:42 Gordon: [Do] you guys have enough to keep you busy for a few days then?

079:34:48 Scott: Hey, Dick, we've got enough to keep us busy for months, and months, and months, as you well know.

[Dick Gordon, Commander of the backup crew has joined the conversation and, as CMP (Command Module Pilot) on Apollo 12, has already witnessed the spectacle of the lunar surface from orbit.]

[When small meteorite impacts excavate through the Moon's blanket of ground-up debris, known as the regolith, and on into bedrock, the resulting crater walls often exhibit a "bench" where the bedrock is exposed. However, the "benches" Dave is describing are "terraces" caused by slumping of the walls of large craters over geologic time due to deep, steeply-dipping faults in the walls.]

079:36:11 Scott: Houston, just north of Conon, there's a - a great depression in the mountains - a low part of the mountains. In the... The western side of the mountains is exposed to the sunlight, and this reflects back in to the shadowed part of the mountains which - the base - basin, just north of Conon there, is really shadowed by the eastern mountain range; but the reflectivity back from the - the mountains exposed to the sunlight illuminates the - the shadowed area to [the point] where we can pick out craters and ridges and various other topographic features [in the dark]. It's - its really quite interesting. As a matter of fact, just to the... The inner walls or the inner basin of Conon itself is illuminated by its own reflectivity on its western wall.

[Conon is named after a Greek mathematician and astronomer, c. 260 B.C.E., and lies about 120 km south of the landing site amongst the disturbed landscape which forms the radial 'sculpture' behind the chain of massifs of the Apennine Front. This landscape is similar to Dave's "Crackled Hills" and originated as the ejecta blanket that swept over the early lunar surface a moment after the impact that formed the Imbrium basin. The dominance of the Imbrium event can be seen by similar landforms across one half of the Moon which all point to the Imbrium Basin.]

[Midway between Conon and the landing site there is indeed a lower section of the Apennine mountain range which includes the arcuate cleft Bela. Measuring 11 by 3 km, Bela appears to have been the source of the lavas which ran through Hadley Rille.]

079:37:30 Scott: Well, we can just barely see subtle features now, I think. We can see the horizon quite clearly.

079:37:43 Henize: Roger. When you get dark-adapted, it may be that things will come through pretty well.

079:37:51 Scott: Roger.

[Very long comm break.]

[Although the western half of the Moon's near-side is not being illuminated from the Sun, it does receive a significant amount of light from the Earth, an illumination visible even from the home planet. Earth not only presents a disk four times larger than the familiar lunar disk, it also reflects about 4 times as much light, due mainly to its clouds.]

[As part of the calibration of the Gamma-ray Spectrometer, the Gain Step Shield, a section of the instrument which discriminates between true detection of gamma-rays and the detection of cosmic-ray particles, is switched off for ten minutes.]

[There are two expected sources of gamma-rays that this instrument is designed to detect. The nuclei of some elements in the lunar surface, particularly iron, will react to cosmic-rays and emit gamma-rays of a precise energy. Other elements, especially Potassium, Thorium and Uranium, emit gamma-rays in the process of radioactive decay and these emissions are also of a well known energy. In association with data from the other instruments, a picture of the composition of the Moon along the ground track can be built up.]

[The Gamma-ray Spectrometer is a scintillation device that detects radiation in the energy range of 1 MeV to 10 MeV. A cylinder of doped sodium iodide reacts to a coincident gamma-ray by converting some of its energy to light which is detected by a photomultiplier tube. Around this cylinder is a light shield, then a plastic shield which detects charged particles but not gamma-rays by means of another photomultiplier tube. The instrument is deployed on the end of a 7.6 metre boom to remove it from contaminating sources around the spacecraft. Apollo 15 is the first mission to carry this instrument. As well as its lunar tasks, it will also be used, during the trans-Earth coast, to monitor the gamma-ray flux coming from sources outside the Solar System.]

079:48:27 Henize: 15, this is Houston.

079:48:32 Irwin: Roger. Houston, 15. Go.

079:48:35 Henize: Jim, the people down here would appreciate it if you could give them something of a description of the operation of the PU valve during the LOI burn.

079:48:51 Irwin: Roger, Karl. There was no operation of the - the PU valve at all until crossover. And then at crossover, it required a - a Decrease, and then at about - about 5 minutes and a half into the burn, it started to increase, and I went to the - the Increase position at that time. All the operation of the PUGS manual operation occurred after crossover.

079:49:26 Henize: Okay; we copy.

079:49:40 Irwin: And, as I mentioned, about 5 and a half, I went to - 5 and a half minutes, I went - went to neutral and then the - it looked like the Unbalance was going to go - it was rapidly departing the zero region, and that was about the time we went through 6 minutes, and I put it into minimum at that time - into the Decrease position.

079:50:19 Henize: Okay, Jim. That answered our next question. [Long pause.]

[The PU (Propellant Utilization) valve was manually controlled by Jim during the LOI burn. He monitored a meter driven by the PUGS (Propellant Utilization Gauging System) and could adjust the flow of oxidiser to the SPS engine to ensure that both propellants were consumed at a ratio of 1.6.]

079:51:16 Irwin: Okay. We were discussing our photography, and we're going to try and stay as close to the preplanned photos as we can and not over extend ourselves into what's already planned for the six days. But we will use our spare - spare film judiciously for the kind of things you hear us talk about that you'd like pictures of.

079:51:37 Henize: Sounds very good.

[Long comm break.]

[

Flight Plan page 3-085.]

[The IMU is being realigned for the first time since entering lunar orbit. This requires two realignments as they are changing their platform's frame of reference from the LOI REFSMMAT to that for the landing site. The first realignment is to the LOI REFSMMAT so that any drift of the platform since the last realignment can be measured and eliminated. Subsequently, another P52 is performed to realign to the landing site REFSMMAT. This latter frame of reference is defined as being the attitude of the landing site at the predicted time of landing. The IMU X-axis is parallel to the landing site's vertical at that time, and points away from the centre of the Moon. The Z-axis is in the direction of flight. This frame of reference is chosen so that after it is transferred to the LM, that vehicle's FDAI display should show 0° in all axes if it lands at the planned time and place and fully upright.]

080:01:50 Scott: Okay. Thank you, Karl. That's good news.

[Comm break.]

080:04:05 Henize: 15. We have your torquing angles.

080:04:12 Scott: Roger. Torqued on the minute.

[Worden, from the 1971 Technical Debrief - "Navigation [in lunar orbit] was about as it was on translunar coast. The guidance system was very tight. I never had any problem getting a star pair. Whether I was doing a slow orb-rate maneuver or whether I was inertial [i.e. in an attitude held with respect to the stars]. P52s worked very well.]

["I still had the problem with the sextant. Even on the back side of the double umbra [where neither the Earth or Sun light the Moon], the sextant was very difficult to use - to identify constellations and to identify the stars. The attenuation in the sextant was really much more than I had anticipated. I could look out a window and see the star field very clearly. In fact, it was much brighter than I expected it to be. There were so many stars in the field of view out the window that, in a way, it was a little difficult to find a constellation and to find the navigation stars. But through the sextant, only the very brightest stars came through. I was able to identify the stars after a while, after I was used to the star pattern, and I did the alignments just about the same place every time."]

[From the 1971 Mission Report - "The flight anomaly [in the optics] was reproduced in the laboratory by placing the optical unit assembly, the removable eyepiece, and the optics panel in a chamber, wherein the environmental conditions that existed in the cabin during flight were duplicated. Condensation on the eyepiece window and, to a lesser extent on the prisms in the removable eyepiece caused the transmittance to decrease to about 4 percent"]

[Worden, from the 1971 Technical Debrief - "Even with the light attenuation through the telescope, the guidance system was so tight that every time I did a P52, I could look through the telescope and grossly identify where I was in the sky. Then when I looked in the sextant, there would be a star right in the middle of the sextant every time. It maintained its orientation beautifully the whole time. The drift rates were very low.]

["The only thing, I guess, that I'd want to comment on concerning navigation, and that in regards the Flight Plan, is that, when we did an Option 1 reorientation, for example, to the plane change attitude, there was no place in the Flight Plan to write the gyro torquing angles for the second P52. Of course, each of these is done with an Option 3 realignment for drift reasons, and those gyro torquing angles are recorded. But then, when you do the Option 1 to go to the new orientation, there's no place in the Flight Plan to record those. I guess there may not be any valid reason to keep those gyro torquing angles. Possibly the ground doesn't need them, but I was in the habit of writing down the gyro torquing angles, and when I got to the Option 1, I did just this. I recorded them in a blank place in the Flight Plan. I feel that we might consider putting those in the Flight Plan, because they are some indication as to how the coarse align works.]

["This reminds me that, on each of the reorientations, I used a coarse-align option in P52, and in each case, the coarse align was good enough to put the star in the sextant, except for one instance on the way back home when we went to entry orientation. The star was just outside the field of view of the sextant, and I had to look for it a little bit. However, the coarse align worked very well. In almost every case, it put the star within half a degree of the center of the sextant."]

[Very long comm break.]

080:13:49 Scott (onboard): ...says it's just ... - He got word from the back room that Farouk and his boys are ecstatic. And the SIM bay stuff is all working very well.

080:14:06 Scott (onboard): (Laughter) Good old SIM bay working up in there and he's jumping up and down. Well, the tape motion is going as planned. Even a little early. Okay.

080:14:36 Scott (onboard): ...? No, I don't think we have time then ... have to get that ... in .... ? You'll spoil the eat period by messing with the...

080:14:54 Scott (onboard): Okay, 10 minutes before the dump, Jim.

080:15:14 Scott (onboard): Man, is that full.

080:15:20 Irwin (onboard): ... DOI.

080:15:37 Worden (onboard): Hopefully, DOI is just going to be a bank B burn. Is that right?

080:15:41 Irwin (onboard): ...

080:16:13 Scott: Houston, Apollo 15. Go.

080:16:17 Henize: Just to firm up our interest in those swirls on the floor of Crisium, the words we'd like to send up is that it'd be nice to get a 3 photo convergent stereo sequence on it, and if you'd like a setting, we recommend...

080:16:33 Scott: Okay; 3 photo; go.

080:16:36 Scott (onboard): You son of a ... bitch! He always stops.

080:16:56 Scott (onboard): I'm going to give Karl about 6 seconds every time, before I answer.

080:17:09 Henize: Roger. And now, you wanted us to remind you about your helmet and gloves when you take shots of Ingenuity this time around.

080:17:24 Scott: Okay; we'll tell him.

080:17:27 Scott (onboard): You wanted to be reminded about helmets and gloves as you take your shots of Ingenuity on this time. What the hell does that mean?

080:17:42 Scott: Okay. Thank you, Karl. We will.

[Very long comm break.]

[As will be normal prior to LOS, the DSE is checked for proper operation. It will record spacecraft telemetry so that on AOS, Mission Control can view the spacecraft's performance during the loss of communication. It will also record the crew's conversations and observations.]

[The spacecraft's orbits about the Moon are counted from the LOI burn and so the spacecraft will begin its second orbit, or "rev 2" while behind the Moon.]

[During this pass over the far-side and the early stage of the next front side pass, the Flight Plan calls for the crew to take photographs as part of the mission's orbital science brief. The targets are Mare Ingenii (Sea of Ingenuity, 33 frames), Keyhole (5 frames), The Bright One (12 frames), Ibn Yunis (14 frames) and Posidonius (21 frames) using the onboard Hasselblad camera with a 250 mm lens and the colour daylight film in magazine M.]

[Exact correlation of the Apollo 15 photograph collection with the timeline is impossible. However, it is probable that a number of images were taken during this far-side pass because by tomorrow, many features will have gone into lunar night. AS15-91-12374 to 12379 look obliquely southwest while the spacecraft is approximately over the unusual dumbbell shaped crater, Van de Graff.

12374 takes a closer look at the rim of the Mare Ingenii basin and a meandering rille which snakes along the mare's shoreline. 12375 is an oblique shot of Mare Ingenii, its huge internal filled crater, Thompson, and the fresher crater, Zelinskij, that obscures its northwest rim. These are the only photographs taken of this mare during the mission. As the spacecraft moves further west, 12376 looks along the northwest rim and a very oblique angle of O'Day, 80 km in diameter with a central peak and three younger craters puncturing its rim. AS15-91-12380 is taken from directly over the large far-side crater, Gagarin, and looks to the southwest horizon at Pavlov and, on the right-hand edge of the picture, Levi-Civita.]

[Flight Plan page 3-086.]

081:11:31 Henize: 15, This is Houston.

081:11:39 Scott: Roger, Houston. Looks like we're getting locked up now.

081:11:42 Henize: Roger. That looks better now.

[Long comm break.]

[The HGA (High Gain Antenna) is being repointed at the Earth. This is achieved by setting it to a wide beamwidth and manually adjusting its direction for maximum signal. Then, on switching the antenna to "Reacquire", the control electronics will begin homing in on Earth. With a good lock achieved, the beamwidth is narrowed to improve the received signal strength.]

081:15:19 Henize: Go ahead, 15.

081:15:28 Scott: Okay, Karl. While I [have] got a minute here waiting on Crisium to show up, I'll give you a run down on what we've done so far.

081:15:36 Henize: Go ahead.

081:15:41 Scott: Okay; we got the strips of photos of the Sea of Ingenuity - or Ingenii - and took a look at the light colored swirls in the bottom of the mare. I couldn't tell - no elevation associated with those light-colored swirls, and they're very distinct when you look at them at this angle. Also - looked at the - at the area just adjacent to Ingenii; there is a very definite valley that cuts through the edge of the wall there, and with what looks like a rille in the bottom [AS15-91-12374], what's been described as Vallis Alpha Reed - I guess it is kind of unique; it's the only one we've seen on the back side so far. We took some pictures of the rim deposits and then took a couple of shots going on out to Dumbbell. After that we got set up for a Keyhole, took some convergent stereo on Keyhole, and got a couple of shots of The Bright One, along with some - some general pictures to show the ejecta pattern, although I'm afraid that ejecta pattern on The Bright One is not going to show up too well. It's - it's very bright but it's - it's also such a large area that it's kind of indistinct as to definition. And then - took a couple of what I hope will be convergent stereos of the - of the rooster tail along by Tangor and then got on to Ibn Yunus/Al-Biruni/Goddard complex and took some convergent stereos of the swirls to the - to the west of Ibn Yunus and to north and west of Goddard. And now we're looking for the ones in Mare Crisium.

[I asked Dave if he could help identify some of the features mentioned in this transmission in light of the crew's practise of using informal names.]

[Scott, from 1998 correspondence - "I would need to review the whole scene - its been a long time! And its sorta like asking about the slope and shape of the 7th mountain peak in Tibet....! Also, here again, Al may be the best source for this, and this transmission may actually have been his? A comment tho' - that first far-side pass is a mindblower - hard to do much but just stare in awe! Another more technical comment here - the readers may not realize that the Hasselblads did not provide time tags as even the least expensive cameras do today - thus an amplification the remark '...correlation of.....with the timeline is impossible."]

081:17:39 Scott: Well, it does look - sometimes brown, sometimes gray, Karl. But we'll see when we get back.

081:17:47 Henize: Hey, let's keep those colors straight, fellows.

[Comm break.]

[The photographs of the Ibn Yunus/Al-Biruni/Goddard complex cannot currently be located in the Apollo 15 collection.]

[Dave has reported seeing swirls on both Mare Crisium and Mare Ingenii. Subsequent to the Apollo 15 mission, many theories have been put forward to account for them but the favoured hypothesis relates them to variations in the magnetic fields of local rocks interacting with the solar wind. It has also been noted that the major concentrations of swirls occur at the antipodal (opposite) points on the Moon from major impacts such as the Imbrium event. Paul Spudis is a geologist at the Lunar and Planetary Institute.]

[Spudis, from 1999 correspondence - "This is the favored Lon Hood explanation, but it is lacking in many respects. First, the biggest swirl (Reiner Gamma) is not antipodal to any basin. Second, the swirls do not have a composition different from their surrounding basalts, so whatever they are, they are not a deposit on something else. The swirls remain mysterious in many respects."]

[Comm break.]

[The HGA is articulated and, driven by its control electronics, can point anywhere within a hemisphere around one side of the SM (Service Module). In Auto mode, it will attempt to track Earth as the spacecraft's attitude changes.]

081:21:28 Scott: Roger. Reacq.

[Comm break.]

[In Reacq(uire) mode, the HGA will also attempt to track Earth. However, should it lose lock on its target, it will slew to angles which have been preset on the Main Display Console.]

081:22:49 Henize: 15, go ahead.

081:22:54 Scott: Okay, Karl. Just a couple of general observations on Crisium while we're coming up on it. Proclus coming up from the east is really spectacular, you can very distinctly see the - the difference in the - in the color of the albedo in the excluded zone of Proclus, and as you are coming up across Crisium with Proclus ahead, you can see the ray pattern very distinct - extending out across Crisium - and follow the ray patterns almost as far as you like. And the excluded zone in the - in the ray pattern is just very distinct at this point.

081:23:34 Henize: Excellent. [Long pause.]

081:24:03 Scott: And, Houston, from this angle looking at Proclus about a crater diameter out to maybe a diameter and a half or so, you can see many small bright fresh craters, which appear to be in the general direction of a ray, like part of the ejecta blanket.

081:24:25 Henize: Roger, Dave. You mean to say that these small bright craters seem to be clearly related to the ejecta blanket. Is that correct?

081:24:36 Scott: That's the impression I get. They occur within a diameter to a diameter and a half of Proclus and - they're about the same brightness as the inner walls of Proclus and they're small - just small craters. I don't see any - Yes, I do see one which you might call a loop, which would suggest secondaries. They just seem to lie in the general direction of the rays of the ejecta from Proclus.

[Beginning with studies by Eugene Shoemaker of the crater Copernicus, which became a model for theories of ejecta dynamics, it was noticed that many of the smaller craters on the Moon were the result of impacts of material that had been ejected from larger impact events. As you would expect, these were called secondary craters. Beyond the rimside ejecta blanket, many chains of secondary craters would be found, often forming distinctive loops.]

081:25:16 Irwin: They're sort of localized to one area which is - probably - yes, on the - on the western side of Proclus, northwest side.

081:25:32 Henize: We copy that. [Long pause.]

081:25:58 Henize: Do you - do these small, bright craters have more or less a uniform size or do they come in varied sizes?

081:26:10 Irwin: I'd say - Karl, this is Jim - I'd say they're various sizes.

081:26:17 Henize: Okay.

081:26:22 Irwin: It is - I - I guess it depends, Karl, on - what do you mean by sizes. There are various sizes within a certain sorting. They - they seem to be fairly well sorted within one range, but within that range, there is a distribution. And they're all much, much smaller than Proclus.

081:26:44 Henize: Okay, we copy.

[Comm break.]

081:28:15 Worden: Roger. You have it.

081:28:18 Henize: And, 15, we don't require a PIPA bias check at this time. And I have a terminator photo PAD when you're ready to copy.

[Changes in velocity due to powered flight (as opposed to changes in velocity due to free fall in a gravity field) are measured within the spacecraft with a type of accelerometer called a PIPA (Pulse Integrating Pendulous Accelerometer). Under free fall conditions the output from the device is not precisely stable but drifts slightly, biasing the overall calculated velocity of the spacecraft. Regular checks are made to ensure this bias is compensated for. Much of the drift in the accelerometers was established before launch, using data collected during pre-flight qualification and acceptance tests. This drift rate is incorporated into the data that the PIPAs are sending to the computer. After launch, small variations in this pre-determined rate are usually observed, and as a result, the expected drift rate is updated.]

081:28:52 Worden: And I'm ready for the terminator photo PAD, Karl.

081:28:52 Henize: Roger. The T start is 81:44:10, and there's a note here that the PCM cable may not reach to window 3. And if it doesn't, go ahead and run on the intervalometer alone. And this pertains to all future photography in window 3.

[Window 3 is the central, circular window which is mounted in the Command Module's main hatch.]

[The lack of a PCM (Pulse Coded Modulation) cable long enough to reach from one of the outlets on the wall to the middle window was first discussed at

032:14:19 when the crew tried in vain to find one to carry out a test of photography through the sextant.]

081:29:43 Henize: 15, we'd like to go to Auto again [on the High Gain Antenna], and go directly from Reacq to Auto without a pause.

["Reacq" and "Auto" are at either end of the HGA Track switch, with "Manual" in the middle. It may be that by pausing in the middle, the control electronics temporarily lose lock on the Earth.]

081:30:07 Henize: The High Gain looks good this time; thank you.

081:30:13 Scott: Roger. [Long pause.]

081:30:46 Henize: 15, Houston. When you can copy, I have both a DOI [Descent Orbit Insertion] PAD and a TEI-5.

[The TEI-5 PAD will come later. It is an abort PAD for an early return to Earth at the end of Apollo 15's fifth revolution around the Moon.]

081:31:08 Scott: Okay. I'm ready to copy the PADs.

081:31:14 Henize: Roger. DOI; SPS/G&N; 39800, plus 1.68, minus 0.55; 082:39:48.29; minus 0208.4, minus 0048.0, plus 0002.0; 000, 283, 347; 0058.4, plus 0009.2; 0213.9, 0:24.5, Delta-Vc is 0208.4; 33, 144.2, 35.7; the rest is NA. Set stars, Vega and Deneb; 288, 340, 346. Ullage is 4 quads, 15 seconds - 15 seconds.

081:33:02 Henize: And the computer is yours.

081:33:09 Scott: Okay, Karl, if you're ready, here's the readback for the DOI PAD. SPS/G&N; 39800, plus 1.68, minus 0.55; 082:39:48.29; minus 0208.4, minus 0048.0, plus 0002.0; 000, 283, 347; 0058.4, plus 0009.2; 0213.9, 0:24.5, 0208.4; 33, 144.2, 35.7; Vega and Deneb; 288, 340, 346; 4 quads, 15 seconds.

[On the early Apollo landing missions, the DOI maneuver was carried out by the Lunar Module's Descent Propulsion System (DPS - pronounced 'dips'). From Apollo 14 onwards, the SPS engine was used for the task, conserving LM propellant and allowing greater landing weight and hover time, if required. With experience, Apollo planners became more aware of SPS propellant usage and were able to refine the margins to facilitate the DOI maneuver.]

[An interpretation of the PAD is as follows:

Purpose: The purpose of the PAD is to put the spacecraft into the descent orbit. With a low point of 17 km near the landing site, this is the orbit the LM will begin its descent from.

System: The burn will be made using the SPS engine under the control of the Guidance and Navigation system.

CSM Weight (Noun 47): 39,800 pounds (18.053 kg). Note that since the LM weight hasn't really changed much (nothing much has been consumed), a previously used value is assumed for it. When the LOI PAD was read up at 074:51:56 and 077:31:04, the weight of the LM was given as 36,258 pounds (16,446 kg). Note also that the NASA documentation listing the nouns available in the computer describes Noun 47 as being the weight of the spacecraft. Strictly speaking, the value relates to the vehicle's mass. Weight is the force applied by a mass in a gravity field. Your weight changes depending on which planet you are standing. Your mass, and therefore your inertia does not.

Pitch and yaw trim angles (Noun 48): +1.68° -0.55°. The thrust axis of the big engine will be set to these angles so that it acts through the calculated centre of gravity of the combined spacecraft.

Time of ignition, T_ig (Noun 33): 82 hours, 39 minutes, 48.29 seconds.

Change in velocity (Noun 81), fps (m/s): x, -208.4 (-63.5); y, -48.0 (-14.6); z, +2.0 (+0.6). These velocity components are measured with respect to the

local vertical/local horizontal. The large negative value of the x component shows that the burn is retrograde, i.e. against their orbital motion. It will slow them down and have the effect of lowering the altitude of their orbit at a point on the other side of the Moon from where the burn takes place. The relatively substantial y component shows that they are changing the orbit's inclination slightly to ensure they will be brought over the landing site at the right time and in the right place. At 085:16:03, Henize explains that there had been a slight error in their state vector when they entered lunar orbit and this out-of-plane component is to compensate for that.

Spacecraft attitude at T_ig: Roll, 0°; Pitch, 283°; Yaw, 347°. These attitude angles are with respect to the orientation of the guidance platform, itself oriented to the

landing site REFSMMAT.

H_A, expected apocynthion of resulting orbit: 58.4 nautical miles. (108.2 km)

H_P, expected pericynthion of resulting orbit: 9.2 nautical miles. (17 km)

Delta-V_t: 213.9 fps (65.2 m/s). This is the total velocity change experienced by the spacecraft.

Burn duration or burn time: 24.5 seconds

Delta-V_c: 208.4 fps. This value is entered into the EMS to allow it to have backup control of the engine.

Sextant star: Star 33 (Antares, in Scorpio) visible in sextant when shaft and trunnion angles are 144.2° and 35.7° respectively.

GDC (Gyro Display Coupler) align stars: Stars Deneb (starcode 43, in the constellation of Cygnus) and Vega (starcode 36, in Lyra) to be used for GDC align in case the IMU is unavailable for this task. The align angles are 288°, 340°, 346°.

SPS propellants are settled in their tanks by firing the plus-X thrusters on all four quads around the Service Module for 15 seconds.]

081:34:17 Scott: All right, go ahead.

081:34:19 Henize: TEI-5, SPS/G&N; 38206; plus 0.58, plus 1.01; 088:25:47.09; plus 2864.3, minus 1227.7, minus 0317.0; 180, 091, 338; the rest is NA. Set stars, Vega and Deneb; 288, 340, 346. 4 jets, 12 seconds. This - Comments are that the burn is undocked and it assumes DOI [has taken place].

081:34:19 Scott: Okay. TEI-5 readback. SPS/G&N; 38206; plus 0.58, plus 1.01; 088:25:47.09; plus 2864.3, minus 1227.7, minus 0317.0; 180, 091, 338; Vega and Deneb; 288, 340, 346; 4 jets, 12 seconds. Undocked and assumes DOI.

081:36:16 Henize: That's all correct. [Long pause.]

Public Affairs Officer - "This is Apollo Control at 81 hours, 37 minutes. CapCom Karl Henize has just read up the information on the Descent Orbit Insertion burn to the crew."

[The PAO announcer is a bit behind events as Karl Henize has just read up the TEI (Trans-Earth Injection)-5 PAD.]

[An interpretation of the PAD follows:

Purpose: This PAD is for an early return to Earth at the end of the fifth lunar orbit in case an abort situation develops.

System: The burn would be under the control of the Guidance and Navigation System.

CSM Weight (Noun 47): 38,206 pounds (17,330 kg). Note that compared to the DOI PAD just read up, this value is smaller to take account of the estimated propellant used during DOI.

Pitch and yaw trim (Noun 48): +0.58° +1.01°.

Time of ignition, T_ig (Noun 33): 88 hours, 25 minutes, 47.09 seconds GET. As with all the TEI PADs, the burn is timed for when the spacecraft is over the far-side.

Change in velocity (Noun 81), fps (m/s): x, +2,864.3 (+873.0); y, -1,227.7 (-374.2), z: -317.0 (-96.6). The large positive x component shows that this burn would be prograde, i.e. with their orbital motion, increasing their velocity so that they escape the gravitational pull of the Moon. The y component indicates that the plane of their orbit would be changed, as would be expected to take them away from their highly inclined orbit to one which includes the Earth.

Spacecraft attitude: Roll, 180°; Pitch, 91°; Yaw, 338°. This would be with respect to the

Landing site REFSMMAT.

Other items, such as the size of the orbit, on the standard form are not applicable (NA) to this PAD or will be taken from previous versions.

GDC align stars: Stars Deneb (starcode 43, in Cygnus) and Vega (starcode 36, in Lyra) to be used for backup GDC alignment in case the IMU is not available. the align angles are 288°, 340°, 346°.

SPS propellants are settled in their tanks by firing the plus-X thrusters on all four quads around the Service Module for 12 seconds.

All these values assume the CSM is no longer carrying the weight of the LM and that they would be aborting the mission from the descent orbit.]

081:37:23 Henize: 15, go ahead.

081:37:29 Scott: Okay, as a quick review here, DOI is a single bank burn on B, with nominal procedures, with the exception of having the A Pilot Valve open.

081:37:48 Henize: That's affirmative, and if we have no ignition, we'll postpone the burn [for) a rev.

[They will use just one of the two available SPS control systems (B) for the DOI burn due to the suspected short-circuit in the other one (A). In the very unlikely event of the SPS failing to ignite, they can wait for another orbit and try again with both banks.]

[Long comm break.]

081:41:00 Henize: 15, this is Houston. We're showing a low voltage on the battery relay bus down here. We think it's just a matter of instrumentation, but there's a couple of procedures we'd like to run through here to check it out.

081:41:27 Scott: Go ahead, Karl.

081:41:29 Henize: Okay; first of all, we'd like read - have an onboard read-out of the battery relay bus voltage, which is B-5 on the test meter.

081:41:43 Irwin: Okay. That's 5-B.

081:41:47 Henize: Roger.

081:41:50 Irwin: It's reading 2.4 - No, I'm sorry, 1.4 - 1.5.

081:42:08 Henize: Roger that reading.

081:42:09 Irwin: Okay, Dave moved the - stand by. Dave wiggled the selector to the right - That's on B and the position that backs the B position and now we're reading 3.5.

[This is a reading from the system test meter which is located in the lower equipment bay, next to the optics panel. Essentially, it is a multifunction meter that displays information from many of the spacecraft's sensors. Most of this information is not so critical as to warrant a dedicated display on the main instrument console.]

[The signals from all the spacecraft's sensors are conditioned so that the desired measurement range is expressed within the voltage range of 0V to 5V. As well as being suitable for the telemetry system to handle, this arrangement allows a single device, the system test meter, to be used for displaying a wide range of sensor readings.

The meter's panel, number 101, has two rotary switches, one marked from A-D, and the other marked numerically from 1-7, plus a transponder setting (XPNDR). A specific test is selected through the two switches, in this case the setting was 5 and B, and the result is displayed on the adjacent voltmeter which has a full scale deflection of 5 volts.]

081:42:37 Irwin: Good.

081:42:55 Henize: Okay; thank you. We'll think on it for a while and everything looks - everything looks fairly normal.

081:43:04 Irwin: Roger.

[Comm break.]

081:44:45 Irwin: B was selected, Karl, but Dave moved the selector out of - just barely out of B and back into the B position to obtain the higher reading.

081:44:55 Henize: Roger. And what about the numerical side; was it in 5?

081:45:01 Irwin: Yes it was.

[As always, when a minor problem appears, the engineers on the ground strive to understand it as completely as possible rather than jump to conclusions. It is likely that a thin layer of oxidation has formed on the switch contacts, adding some resistance to the circuit and just moving the knob has cleaned it off.]

[Comm break.]

[The crew is taking a sequence of photographs at the terminator. These are useful because the lighting angle from the Sun is very low, causing shadows to form on even gentle relief and making the terrain's topography much easier to see. They are using magazine R, which contains very high-speed black and white film, to try and extract as much topographical detail from the images as possible.

AS15-98-13300 to 13302 show the terminator in Mare Vaporum (Sea of Vapours). Relief, especially craters and hills, appears jagged and extreme, suggesting that excessive study of the terminator from Earth-based telescopes is responsible for the mistaken, pre-Apollo notion that the Moon would be a very rough place to explore.]

081:47:59 Scott: Stand by one, Karl. [Long pause.]

081:48:23 Scott: Okay; go with the map update for rev 3.

081:48:28 Henize: Roger. LOS: 82:28:16, 180 [degrees] is 82:48:42, AOS is 83:14:54.

081:48:56 Scott: Okay; understand. LOS: 82:28:16; 180 degrees, 82:48:42; AOS, 83:14:54.

[These are the GET (Ground Elapsed Time) timings for Loss Of Signal, passing over the 180° longitude meridian on the far-side, and Acquisition Of Signal. A box is provided in the Flight Plan on page 3-89 for the times to be written in. They can be used to provide a reference for when they will be flying over various terrain.]

081:49:16 Scott: Okay; go ahead.

081:49:18 Henize: T-Hor [time when J-1 is on the spacecraft's horizon] is 8 - 83:39:33; TCA [Time of Closest Approach] minus 20 [seconds], 83:41:25.

081:49:39 Scott: Okay, understand. T-Horizon at 83:39:33; TCA minus 20, 83:41:25.

081:49:49 Henize: That's correct.

[Long comm break.]

[On the next pass over Mare Serenitatis, Al will use the Sextant to view a landmark, designated "J-1" whose position has been firmly established and whose elevation on the lunar surface has been deemed to be the same as the mean lunar radius (1738.0865 km).]

[Pinpoint landings are very important to the later Apollo missions. While Apollo 11 gave a safe landing a higher priority than an accurate one, subsequent missions wished to explore specific sites. Exploration planning is greatly simplified if the LM can land on target. The location of the target must be well defined with respect to the spacecraft's orbit. As part of this objective, the geometry of the Moon and the spacecraft's orbit will be the subject of close scrutiny leading up to the landing tomorrow.]

[Al will use P24 to control the spacecraft's attitude such that the optics point to where the computer thinks the J-1 landmark is, and if he wishes, he can mark it though he is not required to do so on this attempt. In preparation for this, Karl Henize has just read up the GET of when the crew can expect J-1 to appear on the horizon, and of a time 20 seconds before the spacecraft's closest approach to the landmark.]

081:55:26 Worden: Houston, 15. Go ahead.

081:55:29 Henize: It's our understanding that we'd agreed that you'd send down magazine numbers and final frame numbers on each pass on this photography, and if you're in agreement with that, we'd like to have the magazine and frame number on the orbital photography and also on the terminator photography.

081:55:55 Worden: That - that's all in an agreement that I've got with Spencer, Karl. I think right now, we're too busy to do that, and after we get the landing out of the way, we'll go back and recap all the film and start from scratch.

081:56:07 Henize: Very good.

[Very long comm break.]

[Scott, from 1998 correspondence - "Spencer Gardner (I think), who was in charge of the lunar orbit photo ops, tall fellow, heavy-set, red hair, wore glasses, as I recall - worked on the Flight Crew Support Team."]

[

Flight Plan page 3-087.]

[Apollo 15 is flying over the night time (western) side of the Moon's near-side hemisphere and the crew is involved in routine system checks of the Caution & Warning system, the SPS, the Service Module and Command Module RCS, and the Environmental Control System (ECS). Next, they realign the IMU platform using P52 on option 3. Option 3 is, once again the REFSMMAT option and they use the

landing site REFSMMAT as the orientation to which they align the platform.]

xxx:xx:xx SC: Rog. Torqued on the minute.

082:07:48 Henize: 15, this is Houston.

082:07:53 Scott: Houston, 15.

082:07:55 Henize: One more comment on the battery relay bus voltage. From all indications, it is indeed an instrumentation problem, but we have one more question and that is to confirm that the Main A - Main Bus A and Main Bus B Fuel Cell talkbacks are normal and -and have been normal during this period.

082:08:22 Scott: Yes, that's affirmative, Karl. They have been normal.

082:08:27 Henize: Thank you. And, at the present time, all the systems, otherwise, are looking fine, and you're Go for DOI.

082:08:37 Scott: Okay; understand. Go for DOI.

[Long comm break.]

[The SPS engine burn for Descent Orbit Insertion (DOI) is scheduled 082:39:48. P30 has been executed with all the details of the burn and the spacecraft is being maneuvered to the correct attitude. The Flight Plan calls for VHF omnidirectional antenna C to be used but Karl will ask them to use D for now.]

082:16:50 Irwin: Stand by.

[Panel 226 carries circuit breakers associated with the Electrical Power System.]

082:17:12 Henize: Roger. I understand they have been open. Is that correct?

082:17:19 Irwin: That's correct.

082:17:22 Henize: Okay. The reason we ask is that the temperatures weren't quite as we expected. Thank you.

[The three cryogenic oxygen tanks in the SM contain heaters which, if required, can be used to compensate for the drop in pressure and temperature experienced by the tank as it empties.]

082:17:52 Irwin: Roger. Omni Delta.

[Long comm break.]

[In preparation for the DOI burn, the two experiments running in the SIM bay, the Gamma-ray Spectrometer and the Alpha Particle Spectrometer, have been switched off for now. The Mapping Camera is verified to be in Standby and the Panoramic Camera is switched to Boost, essentially a standby setting. The crew will verify that the DSE recorder is operating before Mission Control lose the data link with the spacecraft. It must record the performance of the SPS engine under single bank control while the DOI burn occurs out of touch of Earth.]

082:26:29 Worden: Roger; understand. And we ran all the systems checks up here, and everything looked good, and I copied the AOS time.

082:26:36 Henize: Excellent.

[Very long comm break.]

[

Flight Plan page 3-088.]

[The spacecraft will commence its third orbit around the Moon half way through this far-side pass.]

[While out of contact with Earth, the only planned item is the DOI burn which is quite critical, so just in case they burn the SPS for slightly too long and lose too much velocity, the Flight Plan includes details of the adjustments they should make if the change in velocity is greater than planned.]

[Since LOI, their orbit has measured about 294 by 109 km (159 by 59 nautical miles) with the high point, or apocynthion, occurring near the landing site at Hadley Rille. The DOI burn will occur at this orbit's low point, or pericynthion, on the opposite side of the Moon from Hadley. The burn, which is intended to slow the spacecraft by 213.9 fps (65.2 m/s), will have the effect of dropping the high point until it becomes the orbit's low point of only about 16 kilometres. Since an accurate landing depends on the precision of this velocity change, the crew must adjust for any errors manually. Also, as there is some uncertainty about the shape of the Moon, and considering that some of the mountains adjacent to the landing site rise 3.4 km (1.8 nm) above the plain at Hadley, burning the SPS longer than planned is particularly undesirable. A small overburn of the 24.5-second SPS firing could risk the spacecraft impacting with the lunar surface.]

[If the velocity is 1 to 2.2 feet per second under what is desired, the minus-X thrusters would be used to increase the stack's velocity (remember, the docked CSM-LM is facing backwards). As these thrusters impinge upon the LM, they cannot be used for larger velocity corrections. The Flight Plan instructs that if the velocity correction is more than 2.2 feet per second, the entire stack should be turned 180 degrees so that the forward facing engines can be used. Correcting for a velocity between 2.2 and 10 feet per second low can be accomplished using the plus-X thrusters. Corrections larger than 10 feet per second are performed using the SPS.]

[In case there is a gross error in the burn which is not picked up by the crew, provision is made for a "bail-out burn". Soon after the DOI burn, the spacecraft is maneuvered into the correct attitude for the bail-out burn should it be needed. Immediately after AOS, Mission Control will use radio tracking information to independently check the geometry of their new orbit. If they are not happy with it they will instruct the crew to carry out the bail-out burn, based on details given at

83:26 in the Flight Plan.]

[After a nominal burn, the new pericynthion will actually be about 250 miles to the east, or uprange of Hadley, and this will be the point from which Falcon's descent will eventually commence in a maneuver called Powered Descent Initiation or PDI.]

[Although many terms are used for the high and low points in a lunar orbit, such as "apolune" and "perilune" or "aposelene" and "periselene" respectively, the correct terms in this context are "apocynthion" and "pericynthion" because they refer to an orbit around the Moon of a spacecraft that came from Earth as opposed to one that was launched from the lunar surface.]

Public Affairs Officer - "This is Apollo Control at 82 hours, 28 minutes. We've had loss of signal on Apollo 15's second lunar revolution. We'll acquire Apollo 15 on it's third revolution after the descent orbit burn at 83 hours, 14 minutes, 54 seconds. If there is no burn, acquisition time will be 83 hours, 11 minutes, 14 seconds. At 82 hours, 29 minutes; this is Mission Control, Houston."

[Flight Plan page 3-089.]

[As with the LOI burn, the time of reacquisition of the spacecraft is greatly influenced by the burn, giving controllers a quick, accurate check of how it progressed. Anything but a nominal burn profoundly affects the exact time the signal from the spacecraft is reacquired.]

Public Affairs Officer - "This is Apollo Control at 83 hours, 9 minutes. We're about a minute 45 seconds away from the no-burn acquisition time. We'll stay up through that period, and up to the normal time. We're about 5 and a half minutes from the nominal AOS time given a DOI burn. ... We've passed the no-burn AOS time now, with no signal. 3 minutes, 30 seconds away from AOS on a nominal burn. We have AOS on the Command Module."

083:09:50 Scott (onboard): ... we can get to this ... The - Can you move that thing?

083:09:58 Worden (onboard): Yes.

083:09:59 Scott (onboard): You really don't need ...

083:10:00 Worden (onboard): Yes.

083:10:01 Scott (onboard): Isn't that the truth? You really don't need it.

083:10:22 Scott (onboard): There it is.

083:10:28 Worden (onboard): ...

083:10:37 Scott (onboard): Wait a minute ....

083:10:43 Worden (onboard): Yes, well, even that ... That's why we had trouble finding anything at all that we could use, because there isn't anything.

083:10:49 Scott (onboard): Nothing to change it over here at all. Nothing to change it, Al, ... that we could use.

083:10:55 Worden (onboard): How about a - Let's see, what kind of ... we use. 25.958?

083:11:01 Scott (onboard): Uh-huh. And We've got ...

083:11:02 Worden (onboard): Yes, and you got ... Five point ... here ....

083:11:14 Worden (onboard): ...

083:11:20 Worden (onboard): ... here ....

083:11:23 Scott (onboard): Huh?

083:11:24 Worden (onboard): .... 3 ...

083:11:33 Scott (onboard): ...

083:11:35 Worden (onboard): ...

083:11:37 Scott (onboard): ...

083:11:39 Worden (onboard): Yes.

083:11:41 Scott (onboard): There'd be a lot more.

083:11:44 Worden (onboard): Yes.

083:12:03 Worden (onboard): ... And - I'm going to push these back in.

083:12:21 Scott (onboard): ... to be all set up with your G&C Checklist ... GDC ALIGN.

083:12:26 Worden (onboard): ...

083:12:36 Worden (onboard): ...

083:12:42 Scott (onboard): ...

083:13:05 Worden (onboard): ...

083:13:08 Scott (onboard): Yes.

083:13:14 Worden (onboard): Got that.

083:13:23 Scott (onboard): I get that initial downhill impression. We're supposed to be ...

083:13:27 Worden (onboard): ... did.

083:13:37 Worden (onboard): ...

083:14:56 Worden (onboard): Darn it. Right there.

083:14:58 Scott (onboard): There it was, whatever it was.

083:15:00 Worden (onboard): Hum ....

083:15:04 Scott (onboard): Yes.

083:15:05 Worden (onboard): Good ....

083:15:24 Scott (onboard): Did you get this ... on, Jim?

083:15:27 Irwin (onboard): Yes, but I never could tell ..., when it went on.

083:15:31 Scott (onboard): Okay.

083:15:33 Henize: 15, this is Houston.

083:15:41 Scott: Hello, Houston, Apollo 15. The Falcon is on its perch.

[Which is another way of saying that they believe they are in the correct orbit for the LM, Falcon, to fly off and do its stuff tomorrow.]

083:15:53 Scott: Okay. Burn status report. Burn was on time. Burn time was about 24.0 - about half a second shorter than predicted. There was no trim; residuals were plus .6 [fps], plus .0, minus .1; Delta-V_c, minus 4.4, fuel 29 - 29.25 [percent of full]; and the oxidizer 29.55; unbalance, 100 increase.

[As it monitored the progress of the burn, the computer decided when there had been enough change in the spacecraft's velocity and shutdown the engine when appropriate which was half a second before the estimated time.]

[Scott, from the 1971 Technical Debrief - "The DOI was again a nominal burn. We shut down on time manually, but the G&N beat us to it. I guess, Al, you could see I put my hands on the switches and timed it. When the time ran out, I put the switches down. Al could watch the P_c [combustion pressure], and I guess he saw it. [To Worden] Why don't you just say what you saw?"]

[Worden, from the 1971 Technical Debrief - "Well, I heard Jim counting down. I knew Dave was ready to throw the switches, and just as his hand started to move, the P_c dropped off. So the automatic shutdown and Dave's shutdown were almost simultaneous; except the automatic shutdown was, I think, just before his. It was perfect."]

[Scott, from the 1971 Technical Debrief - "I took a stopwatch along because we were timing it in tenths of seconds, [which] was necessary for DOI. I think that unless you really have a double failure, you can't get in trouble on DOI, I don't think that is the problem that some people might have thought it was some time ago. That is a good, solid method of getting into a low orbit. Very little chance of getting into a bail-out situation."]

083:16:41 Scott: And I'll tell you, it's really spectacular, when you can see the central peak of Tsiolkovsky coming up over the horizon before you see the rim.

083:16:51 Henize: Hey, that's an interesting astrophysical observation.

[Comm break.]

[Tsiolkovsky is a large, 200-km crater on the far Moon's side which was first photographed by the Soviet probe Luna 3 on 7 October 1959. In the poor imagery of the time, its dark, mare-like interior made it stand out from the other craters that pepper the far-side. The triumphant Soviets, in the manner of all explorers, promptly and appropriately named it after the Polish-Russian pioneer of spaceflight theory, Konstantin Tsiolkovsky (1857-1935). A dominant, W-shaped central peak of light coloured highland material rising out of the dark material makes this crater particularly distinctive and striking and it will be one of Al's major subjects for visual observation during his solo scientific program. As the spacecraft approaches a pericynthion of 18.5 km (10 nautical miles), its altitude is falling and Dave is noticing how the spherical shape of the Moon causes the central peak of Tsiolkovsky to appear to rise above the crater's rim.]

[AS15-91-12381 and

12382 show Tsiolkovsky just after it appeared over the lunar horizon. One of the LM's RCS thrusters obscures the part of the foreground. The comparative height of the central peak is apparent. The viewpoint between the two images is shifted due to the spacecraft's orbital motion. AS15-91-12383 is much closer to the crater and displays the spectacular albedo difference between the dark interior and the light-coloured peak.]

[

AS15-91-12397 was taken later in the mission using a wider-angle lens and looks south into Tsiolkovsky showing the irregular shape of the dark area.]

083:18:08 Henize: We copy, 15.

[Long comm break.]

[After the execution of the burn, the last item detailed in the checklist for the thrusting operations is Verb 16, Noun 44. This command displays the altitudes, in nautical miles, of the orbit's pericynthion and apocynthion, relative to the height of the landing site. It also shows the time taken to make one orbit, the orbital period.]

083:21:29 Henize: We copy, 15.

[A "high-angle pass" comes from a phrase used by tactical fighter pilots.]

[Scott, from 1999 correspondence - "This generally means beginning a steep-angle dive-bombing run, as it might apply to a feature on the surface."]

[As the father of one of the editors of the Apollo Flight Journal is a retired fighter pilot, we thought we would seek his explanation of the term.]

[Lt. Col. Frank J. O'Brien, USAF, Ret. - "A high angle pass is a method of dive bombing that minimizes your exposure to ground fire, and is used for what we called 'slick' bombs, or those with no retarding device. In other words, for all dumb bombs of the 500#, 2000# variety. (When we were dropping napalm or 500# high drag bombs, we used about a 15 degree dive angle and started the run from about 3,000 feet. A lot more exciting experience.) You started by circling the target at about 13-15 thousand feet, depending on terrain elevation and your planned drop altitude. When cleared by the FAC (the Forward Air Controller; a pilot in a small, slow and low-flying aircraft who identifies targets on the ground), you started a diving 90 degree turn to the attack heading, and tried to establish a 60 degree dive angle. Shallower dive angles were not used because of more exposure to ground fire. The first few times you try this steep dive angle it seems a bit hairy, since we trained at George [Air Force Base, in the Mojave desert of California] with 45 degree dive angles, but when they are shooting at you it is a great motivator."]

[Lt. Col O'Brien added that for a more detailed explanation of dive bombing he would refer us to an "excellent work by a little known local author." The title is The Hungry Tigers, the topic in question being on pages 106-122. He did not add that the book was, in fact, written by Lt. Col Frank J. O'Brien, USAF, Ret.]

083:21:45 Henize: True enough. True enough.

083:22:20 Henize: 15, this is Houston. You're Stay in the DOI orbit, and we have an orbit for you of 58.8 by 9.5 [nautical miles, 108.9 by 17.6 km].

083:22:31 Scott: Very good, Houston. 58.8 - 9.5 and we're Stay. Thank you.

[Comm break.]

[On reacquiring the spacecraft around the Moon's eastern limb, the tracking stations on Earth began measuring its velocity and distance from Earth from frequency and delay changes in the received radio signal. From this, they calculated the orbit achieved by the DOI burn. They are in good agreement with the values calculated by the spacecraft's computer. Had Mission Control been unhappy with the orbit, they would have instructed the crew to "bail out". The crew would then have used the emergency burn given at

83:26 in the Flight Plan to alter their orbit.]

[Woods, from 1999 correspondence - "Since the DOI burn has the same effect as the LM DOI burns of Apollos 11 and 12, do you know why they did not have a bail-out contingency when A15 did?"]

[Scott, from 1999 correspondence - "For one thing, with the CSM we could go back up to 60 nautical miles and try DOI again - but with a LM DOI, the LM is committed and the only alternative is an abort. With the CSM, by going to the bail-out attitude immediately, we would be ready for such a contingency and would lose very little orbital motion and timing - to set up a second LOI."]

083:24:06 Scott: Roger, Houston. Thank you.

083:24:08 Henize: And would you please give us Auto on the High Gain [Antenna]?

083:24:13 Scott: Auto.

[Long comm break.]

[Apollo 15's attitude is currently fixed with respect to the stars, and as it orbits, the Moon has gradually moved away from its windows. The "landmark observation attitude" will reorient the spacecraft in preparation for viewing landmark J-1 such that the optics are facing the Moon as they pass over Mare Serenitatis. For a while they can see the Moon's surface again as the spacecraft changes attitude.]

[Dave is literal in his use of "down" as they are approaching their pericynthion and are descending as they cross Mare Crisium.]

083:30:16 Scott: And it looks like we have enough altitude to get up over the [mountains on the] western rim!

083:30:20 Henize: You know, I sure hope so.

083:30:34 Scott: But it sure looks like we're looking up at some of those fellows [the mountains] out there.

083:30:38 Henize: That must be sort of exciting, skimming along down there over the waves.

083:30:46 Scott: That's a mild word for it.

[Woods, from 1999 correspondence with Scott - "Was it the spacecraft's apparent speed that struck you, or a sense of low-flying rather than orbiting or some other impression that prompted your comm?"]

[Scott, from 1999 correspondence - "This comment is due to not so much the speed, as speed is not apparent when still that high over the surface - its the elevation, or angle, of the horizon (mountains) above the 'normal' horizon, whereby the horizon is now higher in the window due to the mountains."]

083:31:02 Scott: No, we're too close. And right now I've just finally picked out the rim of Proclus, and we're just about level, altitude-wise, with the - the rim of Proclus. I cannot see down into it. I can see just a tad of the southern wall. I guess we're just north of it. I can see some large blocks on the outer wall.

083:31:24 Henize: Roger.

083:31:28 Scott: But I'd say we're definitely at an altitude even with the top of the rim of Proclus.

[Long comm break.]

[Dave's comment illustrates the low altitude of their flight path at this point, and their altitude is dropping yet as they approach their pericynthion just east of Hadley. However, they are not really as low as the rim of Proclus. Rather, the curve of the Moon between them and Proclus means that the crater, sited south of them, will be slightly tilted away from them.]

083:36:20 Henize: Roger, I suspect that's Littrow Rille.

[Although Littrow Rille is beyond the shore of Mare Serenitatis, its arcuate form, roughly parallel to the basin rim, suggests it is related to Serenitatis as a result of extensional tectonics, probably as a result of sinking of the mare basalt.]

083:36:56 Scott: I doubt it, Karl. At this attitude for the landmark tracking, the windows are almost out of it. Jim's got some visibility out window 5.

[During landmark tracking, the crew uses the 28-power sextant to view the lunar surface. Since the sextant has a limited field of view, the spacecraft must have the optics pointed towards the surface, and, unfortunately for the sightseeing crew, the placement of the optics, on the opposite side of the spacecraft from the windows, leaves the blackness of space as almost their only view.]

083:38:34 Henize: Roger, 15, we copy.

083:38:46 Henize: Are those ridges smooth, or do they show signs of lots of cracks in them?

083:38:54 Scott: I was impressed with the smoothness of the - the raised portion.

083:39:02 Henize: Roger.

[Dave is describing Dorsa Smirnov, a very prominent ridge running about 130 km in a roughly north-south direction across the mare as they view it. From further away, the ridge is seen to form an arc which is concentric with the rim of the Serenitatis basin. Henize is prompting him to look for features which will pin down their origin, now known to be the result of compression.]

[Mare Serenitatis exhibits some of the best examples of wrinkle ridges and arcuate rilles on the Moon. These features are related and both are caused by the sinking of the relatively dense mare lavas with respect to the surrounding terrain. The centre of the mare sinks further than the edges. In the case of Mare Serenitatis, there is a smooth drop of 200 metres from the shore to the centre. Wrinkle ridges form where compression of the mare surface takes place and causes uplift. The very centre of the mare may display a circular formation of wrinkle ridges which can be mistaken for a ghost crater. Radial ridges may also form. Sometimes wrinkle ridges can betray the existence of features in the basin, especially ancient crater rings, now overlain by the layers of solidified lava which filled the basin to form the mare.]

[Both inside and outside the mare shore, rimae or rilles are often seen running roughly parallel to the basin rim, forming arc-shaped grooves where expansion has occurred. Often the land between two parallel faults drops slightly to produce a feature known as a graben. Rimae Littrow, mentioned by Dave before he reached Serenitatis is a good example of this type of rille.]

[Jim may be referring to AS15-91-12398 which looks backwards to the west towards Dorsa Aldrovandi (named after a 16th century Italian naturalist) with the spacecraft's window obscuring part of the frame. The flooded crater le Monnier is visible on the left of the image. 12399 shows Dorsa Smirnov snaking past an isolated 5.1-km crater named after the American astronomer, Frank W. Very (1852-1927). Photograph 12400 is taken on the western side of Serenitatis. It shows the 3-km crater Hornsby and another small crater, Aratus C, on either side of the image. Faint traces of Dorsum Owen lead to an irregular sunken feature in the middle of the frame, Krishna. Thomas Hornsby was an 18th century British astronomer and George Owen was a 17th century British naturalist.]

[Readers should note that many of the smaller craters on the Moon visible from Earth are given the name of a prominent adjacent crater followed by letters of the alphabet. Aratus C is 130 km east of Aratus.]

083:39:49 Irwin: In the one we just passed over, there were some vertical fractures, definite vertical relief, in the smooth portion of the raised wrinkled ridge. The fractures were also running north and south.

083:40:07 Henize: Roger, Jim. We copy.

083:40:43 Irwin: Roger. It's a spectacular view as we glide across the Sea of Serenity, and I'm taking a picture now of a sinuous rille out to the north.

083:40:55 Henize: Roger, Jim.

[Comm break.]

[Al is attempting to track landmark J-1, a feature on the surface of Mare Serenitatis just east of Dorsum Owen, to check the accuracy of the guidance system's knowledge of the spacecraft's orbit.]

[The spacecraft is approaching its 18-km pericynthion. To make an earthly comparison, the supersonic aircraft, Concorde, cruises at about the same altitude above the Earth, but Apollo 15 is travelling three times faster at 5,960 km/h.]

[This ridge is an exception to the predominant north-south run of ridges in this area of the mare. It may reflect subsurface structure connected with the hills to which it is joined.]

083:42:32 Henize: Go ahead Al.

083:42:36 Worden: Okay, Karl. I just finished the observation on J-1, and everything looked fine from my standpoint. [I] could track it very smoothly. And in fact, I took a couple of marks on it, if anyone's interested.

083:42:51 Henize: Very good, and we have them down here.

083:42:56 Worden: Okay.

083:43:07 Henize: We were sitting down here wondering how you were ever going to find that little bugger. No trouble, huh?

083:43:18 Worden: Not that much trouble, Karl.

083:43:20 Henize: Very good.

083:43:21 Worden: Seemed like there was plenty of time waiting on it. [Long pause.]

083:44:25 Henize: 15, does it look like you are going to clear the mountain range ahead?

083:44:33 Irwin: Karl, we've all got our eyes closed. We're pulling our feet up.

083:44:44 Henize: Open your eyes. That's like going to the Grand Canyon and not looking.

[Comm break.]

[The mountains of the Apennines reach almost a quarter of the spacecraft's altitude and the sensation of speed is enhanced by their proximity to the surface.]

[Bodies in elliptical orbits, like Apollo 15's descent orbit, move faster when they are nearest to the object around which they are orbiting. However, compared to the size of the Moon, the difference between their pericynthion and apocynthion heights is small with little difference in their absolute velocity between these points. However, their close proximity to the Moon does affect their apparent speed. At apocynthion, 110 km up, the terrain parades past at a gentle 0.1° per second. At pericynthion, only 17.6 km altitude, craters and rilles sweep by at over 5° per second, mountain peaks even faster and, being much lower, the sense of perspective is more dramatic.]

[Al is completing a P52 platform realignment, option 3, using the landing site's orientation as the reference point for the platform.]

083:47:15 Scott: Okay, stand by. We're just noticing the cabin temp here, and also that the outlet temp is up to about - the glycol about - outlet temp's up to about 70[° Fahrenheit].

083:47:47 Henize: We copy, and EECOM says that's normal and they're on their way down now.

083:47:55 Scott: Okay, fine. Thank you.

083:47:57 Irwin: And, Karl, I'm ready to copy the Map Camera PAD.

083:48:01 Henize: Roger. They are in the Flight Plan at 84:32 and 84:39. Mapping Camera: T-start, 84:42:23; T-stop 84:54:14. The Pan Camera times are the same as the Mapping Camera's times and we would like to change the shutter speed at 84:24. Instead of 125th, we want 1/250th at 84:24.

[Camera PADs will become a regular occurrence during lunar orbit when Al will start and stop the two main cameras in the SIM bay, the Mapping Camera (which is two cameras in one; the Metric Camera and the Stellar Camera) and the Panoramic Camera. Most photography with these two cameras takes place just to the daylit side of the terminator to take advantage of the low Sun angle and the long shadows which help to make topographic features stand out. The above times refer to when the spacecraft passes from lunar night to day over the far-side, just as they begin their fourth revolution. The change in shutter speed refers to photography, using the onboard Hasselblad and very high speed black and white film, which will occur at the same time as the Mapping and Panoramic Camera operation.]

083:49:00 Henize: That's all correct.

[Long comm break.]

[Very long comm break.]

[

Flight Plan page 3-090.]

084:15:27 Scott (onboard): Yes.

084:15:28 Scott (onboard): Mark.

084:15:29 Worden (onboard): Okay, let me talk to Karl here for a minute.

084:15:32 Worden: Houston, 15.

084:15:35 Henize: Go ahead, 15.

084:15:40 Worden: Okay, Karl. Got a few numbers for you on the [boom] extension times. We started the whole thing off at 84:06:30, and got the covers open, the Mapping Camera extended, and the extension was about 3 minutes instead of 4. Then we deployed the Gamma-ray and the Mass Spec. booms for barber pole plus 2 seconds [to release the tiedowns]. The Gamma-ray turned barber pole after 6 seconds, and Mass Spec. turned barber pole immediately. And I was suspicious of the Mass Spec., so we tried them again and got the same results. Turned the X-ray, On, at 84:15:10 and Laser Altimeter, On, at 84:15:30.

[The above report is as required in the Flight Plan. Apollo 15 is the first mission to carry the SIM bay and is essentially a test flight for it. Everyone involved is therefore very interested to learn how well it performs, especially its various mechanical devices which have never been tested in the freefall vacuum of space. Throughout, Al will keep a note of the time it takes for the three deployable instruments to extend and retract and Mission Control can watch changes in the current going to the motors to monitor the health of these mechanisms. Al will also keep a note of when the non-imaging experiments are switched on and off. Investigators can then relate their data to the timeline and the absolute position of the spacecraft, a data analysis process that will take months to complete.]

084:16:30 Worden (onboard): Looks like that stuff's working fine. Tch, tch.

084:16:32 Scott (onboard): Great! Super!

084:16:34 Irwin (onboard): Good enough.

084:16:36 Worden (onboard): That's it. Verify DSE tape motion at 84:20, and then we get the cameras ready for terminator photos.

084:16:44 Scott (onboard): That a boy!

084:16:50 Worden (onboard): Pan camera, we go - we already got our terminator photos. Did you get - Let's see, we want mag R. That's this mag here.

084:17:07 Scott (onboard): With the Hasselblad? You got the Hasselblad over there?

084:17:12 Worden (onboard): Yes. And, let's see, we want the Hasselblad 80 millimeter, intervalometer--

084:17:21 Scott (onboard): Let's see, intervalometer's down there, Jim, in the - Let's see - It's in the camera - It's right in front of the camera compartment.

084:17:36 Worden (onboard): Oh, boy.

084:17:38 Scott (onboard): It's right there; that's it.

084:17:43 Worden (onboard): Okay. What do you want to do now, get the Hasselblad?

084:18:01 Unknown speaker (onboard): Jim, you're all right.

084:18:08 Worden (onboard): Well, the way to do that is just to play it straight from now on.

084:18:17 Worden (onboard): ... I need somebody to take care of me.

084:18:25 Henize: 15, This is Houston. Would you verify that the X-ray is On?

084:18:30 Worden (onboard): ...

084:18:31 Irwin (onboard): Yes.

084:18:33 Worden (onboard): ... an earful of that.

084:18:36 Worden: 15, Roger. That's verified.

084:18:40 Henize: Thank you. [Long pause.]

Worden (onboard): Is that right, Dave?

084:18:42 Scott (onboard): Yes.

084:18:46 Irwin (onboard): If ... orders, I can get it.

084:18:49 Scott (onboard): Okay.

084:19:01 Worden (onboard): Man, that's really good and stuck!

084:19:04 Irwin (onboard): ... all right.

084:19:06 Worden (onboard): Pork and scalloped potatoes!

084:19:10 Henize: We have not.

[This may be a miskeying by Karl Henize.]

[Comm break.]

084:20:20 Henize: 15, this is Houston. All systems are looking good down here, and until we tell you otherwise, all the AOS's are as in your Flight Plan.

084:20:35 Scott: Roger.

084:20:36 Irwin: We're ready to go. [Laughter.]

084:20:36 Irwin (onboard): That's right [laughter].

084:20:38 Scott: We both like to hear that.

084:20:42 Henize: Roger.

[Very long comm break.]

[Apollo 15 has gone behind the Moon and will commence its fourth revolution while over the far side. As the spacecraft crosses the terminator from night to day, the Panoramic and Mapping Cameras are activated for 11 minutes and 51 seconds to take advantage of the low angle lighting. The onboard Hasselblad is configured with the 80-mm lens and magazine R, containing very high speed (6,000 ASA) black and white film. Compare this to the film used aboard the Lunar Orbiter probes of 5 years earlier which was rated at only 2 ASA to give it some tolerance to radiation in the lightweight construction of that pioneering series of spacecraft. 6 images are scheduled to be taken right on the terminator. These are AS15-98-13303 to 13308. The compilers of the Apollo 15 Index of 70-mm Photographs guess that the first of these very contrasty images may be of the Montes Haemus, the range of mountains on the rim of Serenitatis, but it seems likely that all six images are of the same, unidentified far-side landscape. AS15-98-13308 is one of the clearest of these images which are otherwise difficult to distinguish. Meanwhile, the crew begin their meal period.]

[With the photography completed, the two booms, each more than 7 metres long, are extended from the SIM bay. One boom carries the Gamma-ray Spectrometer and the other, the Mass Spectrometer. The booms take the instruments away from possible sources of contamination near the spacecraft and this is their first deployment. Again, Al times how long it takes for these to extend by monitoring the talkback indicators adjacent to the deploy switches. He records the results in the Flight Plan. The booms will be retracted during burns as they are not designed to withstand the forces of engine firings.]

[The same ingenious mechanism is employed for both booms.

Each has two spools of tempered steel tape which, when unrolled, form themselves into a 'c' profile; much like the way a handyman's measuring tape unrolls to form a curved cross-section which stiffens it. The spools are arranged so that as the two tapes come off and take up their tubular profile, one does so inside the other. A cable to connect the instrument to the SIM bay is wound around the mechanism's housing and is pulled out around the boom during deployment.]

[

Flight Plan page 3-091.]

[The final task on this far-side pass is to switch the Mass Spectrometer's ion source to Standby. This brings on heaters to drive out gases within the instrument for the next hour until it is switched on at 086:00:00.]

Public Affairs Officer - "This is Apollo Control at 85 hours, 8 minutes. We're about 20 seconds away from Acquisition Of Signal. We'll stand by."

085:10:26 Henize: 15, this is Houston.

085:10:33 Scott: Hello, Houston. Five by [five, meaning 'reading you loud and clear.']

085:10:37 Henize: Roger. Like to remind you to configure the DSE as per the Flight Plan.

085:10:48 Scott: Roger.

[Comm break.]

[Karl is asking the crew to rewind the DSE tape so the ground can play it back to check the spacecraft's performance and collect the SIM bay data gathered during LOS.]

085:13:45 Scott: Houston, 15.

085:13:47 Henize: Go ahead, 15.

085:13:51 Scott: Okay. When we get down to the presleep checklist here in about 50 minutes or so, I wonder if you might give us your best guess on the probability of a DOI trim tomorrow.

085:14:04 Henize: Okay. We'll work on that information.

085:14:11 Scott: Okay. Appreciate it. [Long pause.]

085:14:35 Henize: Dave, we can give you a pretty good guess at that now. It seems to be unlikely that we're going to need a DOI trim. I've got a couple of trajectory numbers here if you'd like to copy them.

085:14:50 Scott: Yes, it'd be interesting. Go ahead.

085:14:54 Henize: Our tracking data tells us that your current orbit is 58.2 by 9.1 [nautical miles, 107.7 by 16.8 km]. And, tomorrow morning at wakeup time, it'll be 58.6 by 8.7 [nautical miles, 108.5 by 16.1 km].

[Events in the Moon's past bequeathed it with a gravity field which, to scientists of the late 1960s, seemed unexpectedly uneven. Regional concentrations of mass intensify the gravity over certain areas. Consequently, the orbits of small bodies like spacecraft are unstable in the long term. Known as "mascons," short for "mass concentrations," they are mostly associated with some of the great circular impact basins (Imbrium, Serenitatis, Crisium and Orientale) and are believed to be primarily due to dense mantle material being brought nearer to the surface by the basin-forming impact events, and, to a lesser extent, by the bulk of dense lavas now lying within those basins.]

[Since mascons are largely on the near-side, they accelerate spacecraft slightly when compared to the far-side. Over time, orbits are modified by being lowered on the near-side and raised on the far-side until, if not corrected, they cause the spacecraft to impact the Moon.]

[No previous spacecraft has matched Apollo 15's ground track and ground controllers have not accurately characterised the effect of mascons on its orbit. Based on what they know, Mission Control estimates the pericynthion of their orbit will drop by 0.7 km to 16.1 km. However, these predictions will turn out to be imprecise.]

[Dave is asking about another parameter of orbital mechanics. If their orbit's inclination is not correct, then when it comes to the time of the descent to the surface, the spacecraft will aim to the north or south of the landing site rather than directly towards it.]

085:16:03 Henize: Dave, your out-of-plane data looks like about 2/10ths of a [nautical] mile [0.37 km] at PDI [Powered Descent Initiation] time.

085:16:13 Scott: Okay; that sounds pretty good. Thank you. [Long pause.]

[Henize does not say whether this error is to the north or south but in 23 hours time, just before PDI, there will be a cross track error of 6.1 km (3.3 nautical miles) to the south.]

[The Gamma-ray Spectrometer is due another ten-minute period when the Gain Step Shield is switched off so the operation of its discriminator can be calibrated.]

085:16:55 Scott: Roger. Hign Gain to Auto. [Long pause.]

085:17:48 Henize: Dave, thinking about trajectories, you probably noticed the out-of-plane part of the DOI [burn]. They're telling me here that you burned a perfect LOI, but the state vector they gave you was slightly in error. So, they got rid of - they - they made corrections for that during DOI so that we're standing pretty close to perfect now.

085:18:13 Scott: Okay. I got to admit we did have some question about that [out-of-plane component] but figured you all had it in hand, as you usually do.

085:18:21 Henize: Roger. Between a perfect crew in orbit up there and a perfect crew down here, we're doing pretty good so far. Knock on wood.

085:18:33 Scott: Yes. We got a few miles to cover though.

[Comm break.]

085:20:40 Henize: Go ahead, 15.

085:20:44 Worden: Okay, Karl. Guess I should bring you up to date on a couple of things here. Everything went as planned on the - on the [far-side] terminator photos. The Pan Camera and the Mapping Camera pass started on time and stopped on time. Turn - Got the Mass Spec. boom deployed and Gamma-ray boom deployed; the Mass Spec. deployed in 2 minutes, 20 seconds; and the Gamma-ray deployed in 2 minutes, 28 seconds. Got the Ion Source, On [means Standby], and the Logic Power, Off, at 85:05. And that brings you up to date.

[The Flight Plan included approximate expected times for the two booms to deploy and both of Al's reported times are about 20 seconds quicker than this.]

085:21:34 Worden: Sure does, Karl. We're interested in what kind of data you're getting down there on it.

085:21:45 Henize: OSO's [Orbital Science Officer's] two-word summary of it is that we're getting "beautiful data". Incidentally, Al, if - if you'd like sometime, let us have, say - 12 to 24 hours operation, would you like to have a summary sometime tomorrow on some of the details?

085:22:10 Worden: Yes, indeed, Karl; sure would.

085:22:12 Henize: Okay; we'll get one together.

085:22:14 Worden: Yes, listen. Skip it tomorrow; and, maybe day after tomorrow, we'll get a summary on that. I'll be kind of interested in how it goes myself.

085:22:24 Henize: Very good.

[Comm break.]

085:25:23 Henize: Go ahead, 15.

085:25:28 Worden: Roger, Karl. For your information, you can see both of the - both of the booms at full extension out of window 5.

[This is quite useful information as it will allow the crew to check by eye that the booms are extending properly throughout the orbital science period.]

[About now, the Mass Spectrometer is powered up, though it will continue outgassing for another half hour. The ion source, which is at the heart of the instrument's operation, has not yet been switched on.]

085:25:42 Worden: Yes; they sure look pretty sitting out there.

085:25:46 Henize: Roger.

[Long comm break.]

[According to the Flight Plan, the Mass Spectrometer Experiment switch was due to go to On at 85:25. At 86:00, the Ion Source is due to be switched to On. It is unclear why the Experiment switch is being put in Standby instead.]

085:34:44 Henize: Thank you, Al.

[Comm break.]

085:35:57 Irwin: Roger, Houston. You've got it.

085:36:01 Henize: And, - if you've finished with dinner up there, and somebody can copy, I have a TEI-12 PAD.

[Both of these requests, the uplink and the TEI-12 PAD, are as directed in the Flight Plan. The latter is another abort PAD which, if required, would be used towards the end of the 12th revolution.]

[Apollo 15 is nearing the Hadley landing site within the Apennine range. These mountains are experiencing lunar dawn.]

085:37:05 Scott: Houston, we're making a low pass over the Apennine [mountains], and they're really something.

085:37:12 Henize: Roger. Do they look like any terrestrial mountains you've ever seen?

085:37:28 Scott: No.

085:37:36 Henize: How about the slopes? Are they generally steeper than you expect, or shallower than you expect on something like the Tetons?

085:37:52 Scott: Say again, Karl. I'm sorry; we were discussing the rille at that time - Hadley, that is.

085:37:56 Henize: Roger. I - I was just trying to get a better feel for how the mountains look. Are there - are they more - more craggy and rougher than something like the Tetons or do they give you some other appearance?

085:38:12 Scott: No. As a matter of fact, from this altitude, even though we're low, they appear to be smooth and rounded. There aren't any jagged peaks that we can see. And even though they're cratered, and rough in texture on a small scale, they really don't look anything like the Alps or the San Juan's or any of the other familiar ranges we know.

085:38:38 Henize: Roger. Is there anything that looks like bare rock on them.

085:38:48 Scott: I think we can see some boulders, but there are no apparent jagged peaks that we can tell or that we can see from this - this particular altitude yet, although some of the - the shadows look fairly sharp.

085:39:02 Henize: Roger.

085:39:05 Scott: And, Karl, speaking of shadows, there seems to be enough light being reflected off the sides of the mountains around to supply some light down on the landing site. And the rille is quite distinctive as we pass right over it.

085:39:20 Henize: Beautiful. That must be an eerie sight in a half-light.

[The middle of the day on the Moon is searingly hot while the night is cold to great extremes. Landing at Hadley is timed so that the Sun will have risen just 12°, giving oblique lighting with lots of shadows and aiding landmark identification during the final phase of the landing itself. It also ensures that, as well as the Sun, the landscape isn't radiating huge amounts of heat to overload the EVA suit's cooling ability. Though the Sun is illuminating the mountain peaks around the landing site, it has yet to reach the plain at Hadley. The crew's ability to see detail in the shadows of the Moon is unmatched by the much narrower dynamic range of their cameras, and part of their brief is to describe that which cameras cannot record.]

[The use of magazine R and its load of very fast black and white film at the last terminator crossing is an attempt to record these details on film.]

085:39:33 Henize: And, 15, you can have your computer back.

085:39:38 Scott: Roger.

[Long comm break.]

085:44:09 Henize: 15, this is Houston. How do you read.

085:44:14 Worden: Loud and clear, Houston.

085:44:16 Henize: Roger. We've finished picking up data on the Mass Spectrometer. Leave the discriminator as it is, and we're ready to go to put the Experiment [switch] in Standby now.

085:44:38 Worden: Understand; you're ready to put the Mass Spec. in Standby.

085:44:41 Henize: Roger. And then you can start to put the blunt end forward, anytime you care to.

085:44:49 Worden: Roger; we're maneuvering now.

[Comm break.]

[Since 84:00 GET, the spacecraft has been flying "sharp end forward" or plus-X forward attitude with the CM's apex pointing in the direction of flight. Throughout the coming rest period it will be flying in the "blunt end forward" or minus-X forward attitude with the SPS engine facing the direction of flight. This latter attitude is required for the proper operation of the

Mass Spectrometer.]

085:47:05 Scott: Okay. We copy, Karl. We'll give you all three readings.

085:47:09 Henize: Roger. They'll accept them gladly.

[Comm break.]

085:48:38 Worden: Stand by, Karl.

085:49:04 Worden: Okay, Karl. I'm ready to copy TEI-12.

085:49:09 Henize: Roger. TEI-12, SPS G&N; 38110; plus 0.58, plus 1.00; 101:36:08.38; plus 2845.0, minus 0380.2, minus 0063.8; 180, 107, 354; the rest is NA; 4-jet ullage for 12 seconds. And this assumes the burn undocked and no circular burn, and the GET of landing is 196 hours at MPL.

[An interpretation of the TEI-12 PAD follows:

Purpose: This PAD specifies the information required for an early return to Earth, if necessary, towards the end of the twelfth lunar orbit.

System: It would utilise the SPS engine under the control of the G&N system.

CSM Weight (Noun 47): 38,110 pounds (17,287 kg).

Pitch and yaw trim (Noun 48): +0.58° and +1.00°.

Time of ignition, T_ig (Noun 33): 101 hours, 36 minutes, 8.38 seconds.

Change in velocity (Noun 81), fps (m/s): x, +2,845.0 (+867.2); y, -380.2 (-115.9); z, -63.8 (-19.4). These velocity components are expressed with respect to the

local vertical/local horizontal.

Spacecraft attitude: Roll, 180°; Pitch, 107°; Yaw, 354°. These attitude would be with respect to the orientation of the guidance platform.

Other items on the standard form are not applicable (NA).

SPS propellants are settled in their tanks by firing the plus-X thrusters on all four quads around the Service Module for 12 seconds.

The burn would be made after jettisoning the Lunar Module and with the spacecraft still in the descent orbit; i.e. without a circularisation burn having been made.

Earth landing would then occur at about 196 hours into the mission and in the mid-Pacific landing area. Note that this last item was not specified in the TEI-5 abort PAD, read up at 081:34:19 GET.]

085:50:58 Henize: That's all correct. [Long pause.]

085:51:31 Henize: 15, we need the mode switch in Auto please.

085:51:48 Worden: Houston, 15. What switch you talking about, Karl?

085:51:57 Henize: That's the CMC Mode switch. I guess we need to get into Auto before we can execute this maneuver.

085:52:05 Scott: That's affirmative. And I'll go into Auto as soon as I complete the 40 degrees roll.

085:52:10 Henize: Roger.

[Comm break.]

[A fresh lithium hydroxide canister, number 9, is being placed in receptacle A while the exhausted one, number 7, is stowed in compartment B6.]

[Off is the central position of the Ion Source switch between Standby, its current position, and On.]

[Mission Control are requesting that they keep the Discriminator for the Mass Spectrometer in its Low setting because of scattered sunlight causing excessive background counts in the instrument's detection electronics.]

085:55:37 Henize: Roger. And I - I - think you know that we'd probably - that we - we don't want to go into those operations until we have got into the correct attitude.

[Comm break.]

085:58:14 Scott: Houston, 15; go ahead.

085:58:17 Henize: A couple of special notes on the hardware. First of all, on - on the Systems Test meter - we don't fully understand why that switch did funny things for us, and we have some back in - the fairly extensive tests going on down here still trying to understand it. And we suggest that you leave the meter in the 5-B position until we do get some handle on what happened there.

085:58:46 Worden: Okay, Karl. We copy that.

[Even the smallest anomaly in one of the spacecraft's systems is exhaustively analysed to try and ensure there will be no surprises. Both the SPAN (Spacecraft Analysis) room and the MER (Mission Evaluation Room) will be beavering away at diagrams and specifications of the Systems Test Meter switch, as well as working with the spacecraft contractors, trying to leave nothing to chance.]

[As the Mass Spectrometer is intended to sample the very tenuous lunar atmosphere, it is highly susceptible to contamination from the spacecraft. The two large radiators on the spacecraft are designed to lose only a certain amount of heat. As the spacecraft cycles between lunar night and day, a supplemental cooling system mounted on the SM uses the evaporation of water in a vacuum to carry away excess heat, essentially dealing with the temperature peaks. Although the Mass Spectrometer is carried on the end of a boom, it is feared the resulting water vapour cloud from the evaporator would saturate the experiment.]

[Comm break.]

[

Flight Plan page 3-092.]

[86 hours into the mission is the official time for the crew to begin a 7.7 hour rest period. It will be ten minutes before conversation with Karl Henize finishes and they will have a call seven and a quarter hours later. The presleep checklist is being worked on just now which includes reading the status of batteries, RCS tanks and the PRDs.]

086:01:04 Henize: Go ahead, 15.

086:01:11 Worden: Roger. Bat C is 37 [volts]; pyros A and B are both 37.5 [volts]; RCS 83, 82, 82 and 83 [percent]. The PRD readings, 23072, 25014, and 08016.

086:01:56 Henize: Roger, 15. We copy all that. [Long pause.]

086:02:41 Irwin: Roger. Houston, this is 15. The Ion Source is Off, and we're standing by for your word.

086:02:52 Henize: We copy, 15. Stand by.

[Comm break.]

086:04:27 Irwin: Roger.

[Long comm break.]

086:08:05 Irwin: Okay, Karl. Coming at you.

[The E-Memory dump is the final item on the presleep checklist. It allows Mission Control to study the computer's memory and check its contents.]

086:08:20 Irwin: Ion Source going On.

[With the Ion Source, On, the Mass Spectrometer begins full operation which will continue for the next nine hours.]

[Designed to characterise the lunar atmosphere, the Mass Spectrometer measures the atomic weight of the atoms and molecules which enter an aperture on one side of the instrument.]

[When the spacecraft is flown in an attitude that has the minus-X axis facing forward (i.e. the SPS engine bell facing forward), particles from the lunar atmosphere are rammed into an inlet where they are electrically charged (ionised) by electrons from a filament source. A magnet diverts the path of the resultant ion stream towards two detectors. Simply stated, the heavier an atom or molecule, the more resistant its motion is to change by a magnetic field. By measuring the deflection of the particle stream, the masses of its constituent parts can be determined. The two detectors will detect particles in the mass range of 12 to 66 atomic mass units.]

[The inlet is mounted on the opposite side of the instrument from the CSM to shield it from gases emanating from the spacecraft. By changing the angle of attack of the inlet, it is possible to discriminate between CSM contaminants and genuine lunar atmosphere.]

[According to the Apollo 15 Preliminary Science Report, little difference was detected between the inlet pointing into the flight path and pointing into the spacecraft's wake. This implies that most of what the instrument detects is, essentially, pollution from the spacecraft.]

[The later reference work, the Lunar Sourcebook by Heiken, Vaniman and French, elaborates on this by pointing out how longer term surface experiments placed by Apollo 12, 14, 15 and 17 were deluged with contaminants from Apollo operations which made it very difficult to extract natural data from their results. This is hardly surprising considering that estimates for the total mass of the natural lunar atmosphere are around 10 metric tonnes and a similar quantity of gases are released during each Apollo mission, mostly from operation of the descent and ascent engines.]

086:10:50 Henize: 15, Houston. Could you hold off on that until just after LOS.

086:10:58 Irwin: Okay.

086:11:18 Henize: Okay, 15. Our last worry seems to be cleared up down here. We've got nothing more to bother you with, and all we can do is wish you a good night's sleep.

086:11:30 Irwin: Thank you, Karl. Good night.

086:11:32 Henize: Good night.

Public Affairs Officer - "This is Apollo Control at 86 hours, 13 minutes. We have lost the signal now on revolution 4. We've said 'good night' to the crew, [and] don't expect to talk to them until morning. The voice carrier has been turned off. We'll take this line down now at 86 hours, 14 minutes. ... Flight Director Gene Kranz is preparing to relieve Bill [Milt] Windler and his Flight Controller team. At 86 hours. 14 minutes, this is Mission Control, Houston."

[The rest period will continue until nearly the end of revolution 8.]

Day 4: Lunar Encounter	Journal Home Page	Day 5: Waking in the Descent Orbit