List of Illustrations

Figure 1:   Proposed configuration of a clustered booster.



Figure 2:   Thor-Jupiter engine.



Figure 3:   Booster tooling.



Figure 4:   Early H-1 engine.



Figure 5:   Preliminary concept of Launch Complex 34, Cape Canaveral.



Figure 6:   Saturn B.



Figure 7:   Saturn C.



Figure 8:   Vehicles using Titan and Atlas stages.



Figure 9:   Atlas Centaur vehicle.



Figure 10:  H-1 engine in alignment fixture.



Figure 11:  Model of blockhouse at Launch Complex 34.



Figure 12:  C-1 and earlier vehicles.



Figure 13:  Proposed C-2.



Figure 14:  Booster stage (S-I).



Figure 15:  Second stage (S-IV).



Figure 16:  Third stage (S-V).



Figure 17:  Moving Saturn test booster from assembly to test.



Figure 18:  Booster in test stand.



Figure 19:  Booster static firing.



Figure 20:  Model of J-2 engine.



Figure 21:  Assembly of main LOX tank for SA-1 booster.



Figure 22:  Assembly of tanks on SA-1 booster.



Figure 23:  Structural fabrication of SA-1 booster.



Figure 24:  Installation of engines on SA-1 booster.



Figure 25:  Initial configuration of the S-IV stage.



Figure 26:  Construction of service tower and pedestal.



Figure 27:  Unveiling bust of General George C. Marshall.



Figure 28:  Dr. von Braun and President Eisenhower.



Figure 29:  Mr. Glennan, President Eisenhower, and Dr. von Braun.



Figure 30:  Proposed Saturn C-1 Apollo configuration.



Figure 31:  SA-1 checkout.



Figure 32:  Saturn booster recovery.



Figure 33:  C-2 second stage concept.



Figure 34:  Movement of dummy S-IV stage to checkout.



Figure 35:  First horizontal mating of the Saturn vehicle.



Figure 36:  Removal of the booster from the static test stand.



Figure 37:  Salt water test of H-1 engine.



Figure 38:  Facilities construction at Launch Complex 34.



Figure 39:  The barge Palaemon.



Figure 40:  Redesigned tail of the Saturn booster.



Figure 41:  Six-engine configuration of the S-IV stage.



Figure 42:  Artist's concept of Apollo capsule.



Figure 43:  Air transport of S-IV stage.



Figure 44:  Booster simulator being loaded aboard Palaemon.



Figure 45:  Unloading simulator at the Cape.



Figure 46:  Route of the Palaemon to Cape Canaveral.



Figure 47:  Installing dummy S-V in Dynamic Test Tower.



Figure 48:  Positioning flight booster in test stand.



Figure 49:  Configurations of Saturn flight vehicles.



Figure 50:  Separation of upper stages from booster.



Figure 51:  Model of the RL10-A-3 engine.



Figure 52:  Testing of dummy S-IV stage.



Figure 53:  Sacramento test facility.



Figure 54:  Dummy Saturn vehicle in dynamic test stand.



Figure 55:  Tail area mockup.



Figure 56:  Forward interstage mockup.



Figure 57:  The barge Compromise.



Figure 58:  Launch Complex 34.



Figure 59:  Launch Complex 34, blockhouse interior.



Figure 60:  Instrument unit mockup.



Figure 61:  Comparison of Saturn.



Figure 62:  Possible Nova configurations.



Figure 63:  Proposed C-3/Apollo configuration.



Figure 64:  Installation of SA-T2 in static test stand.



Figure 65:  Dr. von Braun, James E. Webb, and Maj. Gen. Ostrander.



Figure 66:  H-1 and F-1 engine comparison.



Figure 67:  Static firing of F-1 engine.



Figure 68:  Proposed solid propellant boosters for large space vehicles.



Figure 69:  Static firing of SA-T2.



Figure 70:  Concept of new static test facility, MSFC.



Figure 71:  Artist's concept of Apollo separation from second stage.



Figure 72:  Concept of Saturn with nuclear powered stage.



Figure 73:  Booster movement to docking facility.



Figure 74:  Payload movement around Wheeler Dam.



Figure 75:  Booster movement around Wheeler Dam.



Figure 76:  S-I and S-IV stages aboard the Compromise.



Figure 77:  Unloading Compromise in Florida.



Figure 78:  First Saturn booster erection at Cape Canaveral.



Figure 79:  S-IV erection at Cape Canaveral.



Figure 80:  Payload body erection into service structure.



Figure 81:  First Saturn assembled on launch pedestal.



Figure 82:  Saturn Launch Complex 37.



Figure 83:  Artist's concept of launch pedestal for Launch Complex 37.



Figure 84:  Michoud plant at New Orleans.



Figure 85:  Saturn SA-1 flight vehicle on launch pedestal.



Figure 86:  Launch of Saturn SA-1 flight vehicle.



Figure 87:  S-II stage cutaway.



Figure 88:  S-IV tankage at SACTO test facility.



Figure 89:  Barge Promise.



Figure 90:  F-1 engine and test stand.



Figure 91:  S-IC stage.



Figure 92:  S-IVB stage cutaway.



Figure 93:  Saturn C-5.



Figure 94:  SA-2 erected on launch pedestal.



Figure 95:  Regional map showing Mississippi Test Facility.



Figure 96:  S-IV all-systems vehicle.



Figure 97:  Construction of Launch Complex 37.



Figure 98:  Launch of Saturn SA-2 flight vehicle.



Figure 99:  Static firing of F-1 engine.



Figure 100: C-1 first stage test stand.



Figure 101: Saturn C-IB vehicle.



Figure 102: Launch Complex 39.



Figure 103: Saturn C-5 launch pad.



Figure 104: NASA Computer Center, Slidell, Louisiana.



Figure 105: C-5 Dynamic Test Tower



Figure 106: S-IV battleship static firing.



Figure 107: S-IC static test stand.



Figure 108: S-II stage assembly and test facility.



Figure 109: President Kennedy visits MSFC.



Figure 110: Installation of 42-foot boring mill.



Figure 111: Mississippi Test Facility.



Figure 112: Dual plane separation.



Figure 113: J-2 test facility.



Figure 114: S-IC stage facility.



Figure 115: SA-5 configuration.



Figure 116: Unloading S-IV stage at MSFC.



Figure 117: Launch of SA-3 flight vehicle.



Figure 118: Vertical Assembly Building at Michoud.



Figure 119: Launch Complex 39 Vertical Assembly Building



Figure 120: SA-D5 booster.



Figure 121: S-IV Dynamic/Facilities stage at Cape Canaveral.



Figure 122: SA-4 on Launch Complex 34.



Figure 123: Saturn vehicles.



Figure 124: S-IC bulkhead gore forming.



Figure 125: F-1 test stand.



Figure 126: S-II Seal Beach facility.



Figure 127: Crawler transporter.



Figure 128: Micrometeoroid satellite



Figure 129: Static firing of S-I-5.



Figure 130: Completed Y-ring at Michoud.



Figure 131: Explosive forming dies.



Figure 132: SA-5 instrument unit.



Figure 133: SA-4 launch.



Figure 134: Facility checkout of Launch Complex 37B.



Figure 135: Checkout of S-IV-5.



Figure 136: Completion of S-IV battleship test program.



Figure 137: Douglas Huntington Beach Facility.



Figure 138: S-IVB forward mockup.



Figure 139: Fabrication and assembly of S-I-8 at Michoud.



Figure 139A: Barrel assembly.



Figure 139B: Lower thrust ring.



Figure 139C: Tail unit.



Figure 139D: Thrust structure.



Figure 139E: Spider beam.



Figure 139F: LOX and fuel tanks ready for clustering.



Figure 139G: Installation of center LOX tank.



Figure 139H: Clustering 70-inch LOX tanks.



Figure 139I: Clustering 70-inch fuel tanks.



Figure 139J: Final assembly.



Figure 140: Pregnant Guppy aircraft.



Figure 141: Saturn V dynamic tower.



Figure 142: S-IC facility.



Figure 143: Assembly of S-I-9 stage.



Figure 144: Dredging at Mississippi Test Facility.



Figure 145: Mating bulkhead to Y-ring.



Figure 146: S-IB stage.



Figure 147: S-IC static test tower.



Figure 148: Construction at Launch Complex 39.



Figure 149: S-IC stage aft area mockup.



Figure 150: S-IV-5 acceptance firing.



Figure 151: MSFC reorganization.



Figure 152: Loading of S-IV stage.



Figure 153: Intertank for S-IC-T.



Figure 154: Experimental firing in sound suppressor development program.



Figure 155: S-II stage activities.



Figure 155A: S-II aft interstage mockup.



Figure 155B: S-II forward interstage mockup.



Figure 155C: S-II bulkhead fabrication building at Seal Beach.



Figure 155D: S-II structural test tower at Seal Beach.



Figure 155E: Bulkhead fabrication area at Seal Beach.



Figure 155F: Gore forming facility at El Toro.



Figure 155G: S-II skate bulkhead welders at Seal Beach.



Figure 155H: Explosive forming die at El Toro.



Figure 156: Erection of SA-5 at Cape Canaveral.



Figure 156A: Instrument unit.



Figure 156B: S-IV-5 stage.



Figure 156C: Hoisting instrument unit.



Figure 156D: Payload adapter.



Figure 156E: Payload.



Figure 156F: Hoisting payload.



Figure 156G: SA-5 at Launch Complex 37B.



Figure 157: S-IVB liquid hydrogen test tank, MSFC.



Figure 158: Michoud mechanic drilling holes in the first S-IC lower thrust ring.



Figure 159: S-II test stand construction at Santa Susana.



Figure 159A: Flame deflector in battleship test stand.



Figure 159B: All-systems test stand.



Figure 159C: Battleship test stand.



Figure 160: Second stage for SA-6 flight being placed in SACTO stand for acceptance testing.



Figure 161: Spider beam mockup for Saturn IB's first, S-IB, stage.



Figure 162: Saturn V booster test stage components.



Figure 162A: Assembly of S-IC test fuel tank.



Figure 162B: Welding S-IC bulkhead.



Figure 163: Assembly of S-II battleship.



Figure 164: First J-2 extended-duration firing test.



Figure 165: MSFC F-1 engine firing test.



Figure 166: Fifth Saturn I flight.



Figure 166A: Launch of SA-5.



Figure 166B: Second stage separation.



Figure 166C: Launch sequence from tower camera.



Figure 166D: Launch sequence from tower camera.



Figure 166E: Launch sequence from tower camera.



Figure 167: Saturn I LOX tank which will be modified for Saturn IB.



Figure 168: Saturn V test fuel tank.



Figure 169: Saturn I second stage production.



Figure 170: S-IVB Dynamics test stage.



Figure 171: MSFC static test stand for Saturn V booster.



Figure 172: Joining Apollo to SA-6.



Figure 172A: Apollo spacecraft for SA-6.



Figure 172B: Mating of spacecraft to SA-6.



Figure 173: S-I-8, first industry-produced Saturn booster, being unloaded from barge at MSFC.



Figure 174: Mockup of instrument unit for Saturn IB and Saturn V.



Figure 175: First J-2 production engine delivered to Douglas.



Figure 176: Moving Saturn V booster tank bulkhead at Michoud.



Figure 177: Sixth Saturn I flight.



Figure 178: Saturn IB and Saturn V progress at time of sixth Saturn I flight.



Figure 178A: Saturn V booster full scale mockup at Michoud.



Figure 178B: LOX tank assembly for S-IVB stage, upper stage for Saturn IB and V.



Figure 178C: First Saturn V second stage, S-II, flight hardware.



Figure 179: On-board camera photograph of SA-6 stage separation.



Figure 180: ST-124 guidance stable platform.



Figure 181: H-1 engine, uprated for Saturn IB booster.



Figure 182: Saturn IB second stages, S-IVB, in Douglas tooling tower, Huntington Beach.



Figure 183: Fabrication of Saturn V.



Figure 183A: Fuel and LOX tanks being built in Huntsville, for the Saturn V first stage, S-IC.



Figure 183B: Structural test stage thrust unit at Seal Beach, for the Saturn V second stage, S-II.



Figure 184: Aerial view of MSFC Saturn test stands.



Figure 185: S-IU-9 checkout.



Figure 186: Chrysler personnel working on S-IB thrust structure at Michoud.



Figure 187: Douglas personnel working on ground support equipment at Huntington Beach.



Figure 188: First Saturn V hardware from Douglas.



Figure 189: Blockhouse activity at SACTO during S-IV-9 acceptance firing.



Figure 190: SA-7 rises.



Figure 191: Saturn IB nonflight instrument unit.



Figure 192: Clustering Saturn IB first stage at Michoud.



Figure 193: S-IB tail section.



Figure 194: S-IB spider beam.



Figure 195: Saturn engine manufacturing by Rocketdyne at Canoga Park.



Figure 195A: J-2 engine assembly.



Figure 195B: F-1 furnace brazing operation.



Figure 195C: F-1 engine assembly.



Figure 196: Bulkhead for Saturn V second stage.



Figure 197: Electro-Mechanical mockup for Saturn V second stage, S-II.



Figure 198: Last Saturn I booster ground test.



Figure 199: Pegasus satellites for last Saturn I flights housed inside adapted service module.



Figure 200: Chrysler Saturn IB booster work.



Figure 201: Douglas S-IVB stage fabrication area.



Figure 202: F-1 engine test at rocket engine test site, Edwards, California.



Figure 203: Mississippi Test Operations.



Figure 203A: Laboratory and engineering building.



Figure 203B: Test stand for second Saturn V stage, S-II.



Figure 203C: Test stand for first Saturn V stage, S-IC.



Figure 204: Recovered cameras.



Figure 205: S-IV-10 being moved to stand at SACTO.



Figure 206: Chrysler Saturn IB fabrication and assembly area at Michoud.



Figure 207: Auxiliary propulsion system for Saturn IB second stage.



Figure 208: First Saturn V booster, a nonflight version for static tests.



Figure 209: First short-duration S-IVB battleship firing.



Figure 210: Buildup of Saturn V second stage, nonflight version for tests.



Figure 211: Pegasus B.



Figure 212: Saturn IB test first stage being readied for shipment.



Figure 213: First Saturn IB test second stage, S-IVB-D, at turnover ceremony at Douglas.



Figure 214: S-IC-S thrust structure on barge at Michoud.



Figure 215: Internal ribs of first Boeing-built Saturn V fin, assembled and ready for attachment of skins.



Figure 216: J-2 engine gimballing test.



Figure 217: Replacement of S-II-S bulkhead.



Figure 218: Saturn stages en route to MSFC by barge.



Figure 219: Pegasus with wings fully extended.



Figure 220: Assembly of S-IU-200D/500D for the Saturn IB and Saturn V.



Figure 221: Cryogenics dock at MTO after completion.



Figure 222: Meteoroid measurement capsule.



Figure 223: SA-9 launch at Kennedy Space Center.



Figure 224: S-II-1 thrust structure fabrication at Tulsa.



Figure 225: S-IC-T en route from ME lab to test stand.



Figure 226: Erection of S-IC-T in test stand at MSFC.



Figure 227: Saturn IB booster being moved into static test stand.



Figure 228: Positioning S-IV on S-1 at KSC.



Figure 229: Saturn IB/Centaur configuration.



Figure 230: Static firing of S-IB-1 at MSFC.



Figure 231: Static test of all five engines of Saturn V booster (S-IC stage).



Figure 232: Deployment sequence of the Pegasus.



Figure 233: S-IVB-201 en route to Courtland, California, aboard the Orion.



Figure 234: S-IVB production sequence.



Figure 235: S-II stage.



Figure 236: Launch of SA-8 from pad 37B at KSC.



Figure 237: Rocketdyne technicians checking out a J-2 engine.



Figure 238: Point Barrow, carrier for S-IVB-500F stage.



Figure 239: Launch complex 34 gantry at KSC.



Figure 240: Pegasus with partial deployment of wings.



Figure 241: Opening of locks at MTF.



Figure 242: S-IB static test, Huntsville.



Figure 243: Saturn SA-10, during countdown demonstration test.



Figure 244: Launch of SA-10 from pad 37B, KSC.



Figure 245: Technicians checking Rocketdyne-built J-2 engines on S-II stage.



Figure 246: S-IC static firing.



Figure 247: Computer room during S-IVB-201 firing at Sacramento.



Figure 248: S-II battleship cluster firing at SSFL.



Figure 249: S-II A-2 test stand, Mississippi Test Facility.



Figure 250: S-IVB-201 being hoisted on the Steel Executive.



Figure 251: Altitude simulation test facility at Tullahoma, Tennessee.



Figure 252: Damage at Michoud by Hurricane Betsy.



Figure 253: NASA barge Promise upon levee after Hurricane Betsy.



Figure 254: Hurricane Betsy leaves Promise on levee.



Figure 255: Aftermath of Hurricane Betsy at Michoud.



Figure 256: S-IB-200D being lifted into dynamic test stand at MSFC.



Figure 257: S-IU-200/500S on fabrication stand No. 1.



Figure 258: Loading S-II-T on AKD Point Barrow.



Figure 259: S-IC-T static test firing.



Figure 260: S-IC-D being unloaded from barge Poseidon.



Figure 261: S-II-T arriving at S-II A-2 stand at MTF.



Figure 262: Installation of S-II-T in MTF test stand A-2.



Figure 263: S-IVB-202 installed in test stand Beta 3 at SACTO.



Figure 264: H-1 engine.



Figure 265: S-II common bulkhead test tank (CBTT).



Figure 266: Major components of J-2 engine.



Figure 267: Apollo capsule.



Figure 268: Studies on reusable transport system.



Figure 269: S-II battleship firing, Santa Susana.



Figure 270: S-IC-D erected in S-IC test stand MSFC.



Figure 271: Barge Poseidon used to move Saturn stages.



Figure 272: S-IC-1 and S-IC-2 in transit at MSFC.



Figure 273: S-IC-T removed from test stand at MSFC.



Figure 274: Moving of S-IVB-501 after post-manufacturing checkout.



Figure 275: MSFC dock activity.



Figure 276: AS-201 awaits launching, KSC.



Figure 277: Instrument unit configuration.



Figure 278: H-1 engine.



Figure 279: Transfer of S-II-F and interstage from dock to VAB, KSC.



Figure 280: S-IU-202 moving to KSC.



Figure 281: S-IC development test stand, Huntsville.



Figure 282: AS-201 launch, KSC.



Figure 283: Uprated Saturn I launch vehicle configuration.



Figure 284: S-II-F stage in Vehicle Assembly Building, KSC.



Figure 285: S-IVB facilities at Huntington Beach.



Figure 286: S-IVB facilities at SACTO.



Figure 287: F-1 engine.



Figure 288: S-IVB-500S/T aboard Super Guppy.



Figure 289: S-IB stage erection in test stand, Huntsville.



Figure 290: J-2 production at Rocketdyne.



Figure 291: RL10 engine.



Figure 292: Final check of H-1 engines before shipment.



Figure 293: Barge Promise.



Figure 294: Super Guppy.



Figure 295: S-IVB stage hydrogen tanks.



Figure 296: S-IVB stage in test stand Beta 1, SACTO.



Figure 297: S-II static firing at MTF.



Figure 298: Static firing of an S-II flight stage.



Figure 299: Saturn V in movement at KSC.



Figure 300: S-IVB-501 acceptance firing at SACTO.



Figure 301: Destroyed S-II-T/D due to overpressurized liquid hydrogen tank.



Figure 302: Loading sequence of Super Guppy.



Figure 303: Saturn V and mobile launcher on crawler emerging from VAB, KSC.



Figure 304: AS-203 flight.



Figure 304A: Launch of AS-203 from pad 37B.



Figure 304B: AS-203 in flight, showing shock wave forming around nose cone.



Figure 305: Acceptance firing of the S-IVB-502 at Sacramento.



Figure 306: S-II facilities at Seal Beach.



Figure 307: Transfer of S-II-1 from Point Barrow to Pearl River at Michoud en route to MTF from Seal Beach.



Figure 308: General view of S-IVB-501 with Super Guppy.



Figure 309: Launch Complex 34, KSC.



Figure 310: Fourth uprated Saturn I, S-IB-4, in first stage of journey to KSC.



Figure 311: S-II-1 arriving at MTF for acceptance testing.



Figure 312: S-IU-501 arrives at KSC aboard Super Guppy.



Figure 313: AS-202 rises from KSC on August 25, 1966.



Figure 314: S-IC-1 stage arrival, KSC.



Figure 315: S-IU-200/500S during structural test, MSFC.



Figure 316: S-IC-3 being loaded on barge Poseidon for shipment to KSC.



Figure 317: S-IC-3 being erected in the static test stand at MSFC.



Figure 318: Checkout of Instrument Unit for Saturn V at Huntsville.



Figure 319: S-II-F stage being unloaded at MSFC.



Figure 320: S-IC test stand at MTF.



Figure 321: F-1 engine checkout.



Figure 322: Cracks in the liquid hydrogen tanks for the S-II-3.



Figure 323: Dynamic vehicle stacked in the Saturn V dynamic test tower at MSFC.



Figure 324: Instrument Unit production at Huntsville.



Figure 325: S-IB-7, S-IB-9, S-IB-5, and S-IB-6 in final assembly area, Michoud.



Figure 326: Saturn V third stage (S-IVB).



Figure 327: AS-503 third stage (S-IVB) explosion.



Figure 328: S-II-1 stage in Vehicle Assembly Building, KSC.



Figure 329: S-IU-1 stage in Vehicle Assembly Building, KSC.



Figure 330: Assembly area, Huntington Beach, California.



Figure 331: S-IVB-505 and S-IVB-211 in vertical checkout tower at Huntington Beach.



Figure 332: Palaemon enroute to MSFC with S-IB stage.



Figure 333: Michoud, aerial view with plant in background.



Figure 334: Aerial view of pad 34 at KSC after fire.



Figure 335: S-IVB-503N in Beta test stand at SACTO.



Figure 336: S-IVB-206 at pad 37, KSC.



Figure 337: Saturn V first stage (S-IC).



Figure 338: Saturn V vehicle configuration.



Figure 339: Saturn V S-IC test stand B-2 at MTF.



Figure 340: AS-501 Instrument Unit in VAB, KSC.



Figure 341: S-IC being transported to MSFC by barge.



Figure 342: S-IVB-206 on transporter in VAB, Sacramento.



Figure 343: S-IVB-206 being unloaded from Super Guppy.



Figure 344: AS-204 preparations.



Figure 344A: Arrival of S-IB-204 at KSC.



Figure 344B: Stacking of S-IB-204 on pad 37B.



Figure 345: Michoud, aerial view of engineering building and manufacturing area.



Figure 346: Barge transportation for Saturn stages.



Figure 347: Rebuilding Beta III test stand at SACTO.



Figure 348: S-IC-8, S-IC-4, and S-IC-6 in manufacturing building, Michoud.



Figure 349: S-IB stage being loaded on barge.



Figure 350: S-IC flight stage, Huntsville.



Figure 351: J-2 engine being moved to test stand for static firing.



Figure 352: Manufacture of Saturn I workshop at Huntington Beach.



Figure 353: Skylab mockup being moved to MSFC.



Figure 354: Saturn IB uprating and developmental studies.



Figure 355: S-IVB acceptance firing at SACTO.



Figure 356: Preparation of F-1 engines for static firing.



Figure 357: Saturn V S-II-2 at KSC.



Figure 358: Mockup of the Saturn I workshop.



Figure 359: F-1 engine.



Figure 360: F-1 test facilities, Edwards AFB.



Figure 361: Stacking of Saturn V AS-501 Apollo 4.



Figure 361A: Placement of S-IC-501 on mobile launcher.



Figure 361B: Stacking of S-II-501.



Figure 361C: Stacking of S-IVB-501.



Figure 361D: Stacking of S-IU-501.



Figure 361E: Stacking of Apollo spacecraft on AS-501.



Figure 362: Saturn V flight vehicle AS-501 in VAB.



Figure 363: S-IVB-209 at Beta I test stand, SACTO.



Figure 364: S-IC-5 leaving MAF on barge.



Figure 365: AS-204 preparations.



Figure 365A: Arrival of LM-1 at KSC.



Figure 365B: Lifting of LM-1 at launch pad for stacking on AS-204.



Figure 366: Saturn V S-IC recovery study.



Figure 367: S-IC-8 horizontal installation at Michoud.



Figure 368: Installing J-2 engine in test stand for static firing.



Figure 369: S-IVB's in storage at SACTO.



Figure 370: Stacking of AS-502 Apollo 6.



Figure 370A: Stacking S-II-2 for AS-502 Apollo 6.



Figure 370B: Stacking S-IU-2.



Figure 371: Saturn V S-IC is transported by barge.



Figure 372: S-IC stages in horizontal area, Michoud.



Figure 373: S-II in S-II A-2 test stand at MTF.



Figure 374: Lowering S-IC onto barge at MTF.



Figure 375: Apollo Saturn V, AS-501 rollout, transfer from VAB to LC-39A.



Figure 376: AS-501 moves up the incline at pad 39A.



Figure 377: Mobile Service Structure at LC-39A for Apollo Saturn 501.



Figure 378: Saturn S-IC components in assembly building at MAF.



Figure 379: Apollo lunar landing mission, typical profile.



Figure 380: Saturn 501 from top of Mobile Service Structure, pad 39A.



Figure 381: AS-501 Apollo 4 flight.



Figure 381A: Launch of AS-501 from pad 39A.



Figure 381B: AS-501 climbs toward orbit.



Figure 382: AS-501 mission sequence.



Figure 383: Installation of S-II-4 in test stand at MTF.



Figure 384: Spacecraft for Apollo 6 in VAB.



Figure 385: Simulation of activities in Saturn I workshop.



Figure 386: S-IVB-206 being unloaded from Super Guppy.



Figure 387: F-1 engine prepared for static firing.



Figure 388: Components and assembly of S-IC first stage at Michoud.



Figure 389: S-IC flight stage at Michoud.



Figure 390: S-IVB's in storage at SACTO.



Figure 391: First stage of AS-503 in VAB, KSC.



Figure 392: H-1 engine.



Figure 393: AS-204 on pad 37B, KSC.



Figure 394: Launch of AS-204 Apollo 5 with LM-1.



Figure 395: Simulated activity in S-IVB orbital workshop.



Figure 396: Saturn V S-II stage on transporter, Seal Beach.



Figure 397: Rollout of Saturn V AS-502 from VAB.



Figure 398: MSS moves back from AS-502 on pad 39A.



Figure 399: Removal of S-II-4 from A-2 test stand at MTF.



Figure 400: S-IC stage at base of test stand, MTF.



Figure 401: S-IC at MTF test stand.



Figure 402: Saturn V AS-502 on pad 39A, KSC.



Figure 403: AS-502 mission sequence.



Figure 404: AS-502 Apollo 6 flight.



Figure 404A: Launch of Apollo 6, Saturn V AS-502.



Figure 404B: AS-502 continues to climb on S-IC thrust.



Figure 405: Saturn IB on pad (AS-205).



Figure 406: Saturn V on pad (AS-503).



Figure 407: Stacking of AS-205 Apollo 7 on pad 34.



Figure 408: Stacking of AS-503 Apollo 8 in VAB.



Figure 409: S-IB-211 being moved to test stand at MSFC.



Figure 410: Apollo 8 lunar mission sequence, orbital mission (AS-503).







Appendix A; SATURN MISSIONS



Figure 1: Saturn I Launch Vehicle



Figure 2: Saturn IB Launch Vehicle



Figure 3: Saturn V Launch Vehicle







Appendix B; SATURN CHARACTERISTICS



Figure 1: Saturn I Launch Vehicle



Figure 2: Saturn IB Launch Vehicle



Figure 3: Saturn V Launch Vehicle







Appendix C; SATURN MAJOR CONTRACTORS



Figure 1: Saturn I Major Contractors



Figure 2: Saturn IB Major Contractors



Figure 3: Saturn V Major Contractors







Appendix D; LAUNCH SUMMARY



Figure 1: Saturn I Launch Summary



Figure 2: Saturn IB Launch Summary



Figure 3: Saturn V Launch Summary







Appendix E; SEQUENCE FOR SATURN V MANNED LUNAR VOYAGE



Figure 1: Sequence for Saturn V Manned Lunar Voyage







Appendix F; SATURN LAUNCH VEHICLE STAGES AND CONFIGURATIONS



Figure 1: Saturn I S-IV Second Stage



Figure 2: Saturn IB S-IVB Second Stage



Figure 3: Saturn V S-IVB Third Stage



Figure 4: Saturn V S-II Second Stage



Figure 5: Saturn I S-I First Stage



Figure 6: Saturn IB S-IB First Stage



Figure 7: Saturn V S-IC First Stage



Figure 8: Saturn IB Vehicle Configurations



Figure 9: Saturn V Vehicle Configurations







Appendix G; SATURN LAUNCH VEHICLE ENGINES



Figure 1: RL-10 Engine



Figure 2: J-2 Engine



Figure 3: H-1 Engine



Figure 4: F-1 Engine



Figure 5: Saturn Engine Applications



Figure 6: Engines for Manned Flights



Figure 7: Launch Vehicle Engines