[85] 6.1. INTRODUCTION
Under present conditions the motion of planets and satellites is not appreciably perturbed by collisions (viscosity). However, in the asteroidal belt and in meteor streams the interactions are in many cases large enough to perturb the motion of individual bodies. During the hetegonic era, when the matter now stored in planets and satellites was dispersed, we can expect that the interaction between grains was of decisive importance.
In ch. 5 we have seen that over a large range of mass the dominating type of motion is a Kepler motion perturbed by collisions. This chapter is devoted to a study of this type of motion, a topic that has previously received little attention. The bodies treated in this discussion are assumed to be large enough that electromagnetic effects may be neglected. In the typical examples treated in sec. 5.4 this condition is that R >>10^{4} cm. Radiation effects are also neglected.
It is shown that under certain conditions collisionperturbed Kepler motion results in the formation of "jet streams," selffocused streams of particle aggregates held together by means of a "dynamic attraction" or "apparent attraction." It is suggested that meteor streams and the asteroidal jet streams described in sec. 4.3.3 may be of this type. It is further argued that jet streams were of decisive importance as an intermediate stage in the accretion of planets and satellites from grains. It will be seen in ch. 22 that in jet streams characterized by collisionperturbed Kepler motion accretion of large meteoroids may take place. It is likely that the jetstream milieu is decisive for the formation of meteoroids, and, vice versa, meteoroids may supply us with important data for the understanding of the evolution of jet streams.
6.2. THE INTERPLANETARY MEDIUM
The small grains of different sizes together with the plasma constitute what is referred to as the interplanetary medium. The presence of this medium means that the motions of small bodies in interplanetary space are [86] influenced by viscous effects. For planets and satellites these effects are so small that they have not yet been discovered (sec. 4.1). For the smaller bodies we are studying in this chapter, viscosity does play a role, the importance of which increases as the mass of the body decreases. In hetegonic times viscosity effects were much more important than now.
It is generally agreed that collisions have been decisive for the evolution of the asteroidal belt. Kiang (1966) finds that a correlation between proper eccentricities and proper inclinations of asteroids suggests the existence (or former existence) of a resistive medium. However, even down to the smallest observed asteroids (R = 10^{5} cm), gravitation is by far the main force, and viscosity only enters as a small correction.
The study of the motion of comets has revealed that forces other than gravitation are sometimes important (Marsden, 1968; Hamid et al., 1968).
It is often implicitly assumed that in interplanetary space there is a "resistive" medium that is essentially at rest. We know that in interplanetary space there is a radial outward motion of a very thin plasma (solar wind), but its density is too low to affect the motion of grains appreciably (its effect is smaller than the PoyntingRobertson effect). Hence, any such assumed resistive medium must necessarily consist of grains. However, an assembly of grains cannot possibly be at rest because the grains are attracted by the Sun. The only possibility is that they are supported by centrifugal force (i.e., they are moving in Kepler orbits).
Hence, a "resistive medium" affecting the motion of the asteroids can be "at rest" only in the sense that on the average there would in principle be an equal number of grains moving in all directions. Observations do not support the existence of such a resistive medium in interplanetary space. It seems likely that, on the average, all small bodies with short periods (i.e., asteroids, comets, and meteoroids) are moving in the prograde sense.
6.3. EFFECTS OF COLLISIONS
Most of the early discussion of the mutual interaction between grains in space has been based on a widespread misconception that we shall discuss in this section.
Suppose that a parallel beam of particles is shot through a particulate medium at rest. Then collisions between the beam particles and the particles at rest will scatter the moving particles. The beam will be diffused so that its particles will spread in space. Almost all treatment of the motion of bodies (grains, meteoroids, and asteroids) in interplanetary space is based on this model although it is applicable only under certain conditions, which are usually not found in interplanetary space.
There is a basic misconception that grain collisions, either with a [87] "medium" or with other moving grains, will lead to an increased spread of the grain velocities and orbits. As stated above, this is true for a beam of particles that is not moving in a gravitational field. It is also true for particles in a gravitational field under the conditions that the time between collisions is smaller than the Kepler period and that the collisions are elastic. The most pertinent case for our studies, however, is that of grains making many Kepler revolutions between collisions that are essentially inelastic. In this case collisions lead to an equalization of the orbits of the colliding particles, with the result that the spread in both velocity and coordinate space is reduced.
Suppose that two particles with masses m_{1} and m_{2} move in orbits with specific angular momenta C_{1} and C_{2} (C_{2}_{ }> C_{1}). According to the guiding center picture, they perform oscillations in the radial and axial directions (sec. 3.3) with amplitudes (r_{1}e_{1}, r_{1}i_{1}) and (r_{2}e_{2}, r_{2}i_{2}), respectively, while their guiding centers move along circles of radii r_{1} and r_{2}.
If r_{1}(1+e_{1}) r_{2}(1e_{2}), the particles have a chance of colliding. If the precession rates of their nodes and perihelia are different and not commensurable, they will sooner or later collide at a point at the central distance r_{3}. At collision, their tangential velocities will be v_{1}_{ }= C_{1}/r_{3} and v_{2}_{ }= C_{2}/r_{3}. If the collision is perfectly inelastic, their common tangential velocity v_{3} after the collision will be v_{3} = (m_{1}v_{1}_{ }+ m_{2}v_{2})/(m_{1}+ m_{2}). Hence, each of them will have the specific angular momentum
which means C_{1}< C_{3}< C_{2}. Collisions that are essentially inelastic will tend to equalize the specific angular momenta of colliding particles. It is easily seen that collisions also will tend to make the particles oscillate with the same amplitude and phase.
From the above discussion, one concludes that the general result of viscosity is to make the orbits of particles more similar. This effect is closely connected with what is termed apparent attraction in sec. 6.4.1.
6.4. ORBITING PARTICLES CONFINED IN A SPACECRAFT
In spite of the fact that celestial mechanics is several centuries old, few, if any, textbooks give a clear picture of some simple cases that are of interest for the present discussion. This is because celestial mechanics is usually [88] presented with a somewhat formidable mathematical apparatus that conceals some important physical aspects of the phenomena. The conceptual approach used here was chosen to clarify and emphasize certain fundamental characteristics of the phenomena under discussion.
Suppose that a number of particles ("apples"; see Alfvén, 1971) are enclosed in a spacecraft that is orbiting around a central point mass M_{c} in a circle of radius r_{0} (measured from the center of gravity of the spacecraft). If the masses of the spacecraft and of the particles are so small that gravitational attraction between them is negligible, all the particles will move in Kepler orbits around the central body. At the same time, they are subject to the constraint that they must permanently remain inside the spacecraft. The confinement of particles in a physical enclosure provides an idealized model of those phenomena which cause the particles in a jet stream to keep together.
We shall study what Kepler orbits are selected by this constraint and how these orbits look, as seen from the spacecraft. We introduce an orthogonal coordinate system with the origin at the center of gravity of the spacecraft, with the x axis pointing away from the central body and the y axis pointing in the direction of motion (see fig. 3.3.1).
The condition that a particle in a Kepler orbit must remain inside the spacecraft necessitates that its Kepler period T_{K} be the same as that of the spacecraft (i.e., its semimajor axis is r_{0}_{ }). The most simple case, the particle being at rest in relation to the spacecraft, occurs when both the eccentricity and inclination are zero. In this situation the particles are located at the distance r_{0}_{ }from the central body (i.e., approximately on the y axis). Hence, the particles in the spacecraft are aligned in the direction of orbital motion along the line (or strictly the circular arc) through the center of gravity of the spacecraft.
6.4.1. Transverse Apparent Attraction
If e = 0 but iO, the particles will move in a circular orbit inclined to the orbital plane of the spacecraft. Seen from the spacecraft, the particle will oscillate in the z direction about its equilibrium position on the y axis. The period of this oscillation is T_{K}. Seen from the spacecraft, the motion of the particle can be described as due to the z component of the gravitational force of the central body:
If eO the particle will move in an ellipse. Seen from the spacecraft, its [89] motion is an oscillation in the x direction with period T_{K}. It can be described as due to a force in the x direction:
However, it is coupled with an oscillation in the y direction with twice the amplitude.
If a large number of particles collide inelastically or if gas in the spacecraft damps their oscillations, the eventual result will be that all the particles are at rest, lined up along the y axis.
Both the oscillation in the z direction and the oscillation in the xy plane can easily be described by the guidingcenter method described in ch. 3. Using that terminology we can state: If particles in Kepler motion are confined inside a spacecraft, their guiding centers will line up along the y axis.
The particles will oscillate about their guiding centers as if they were acted upon by a transverse apparent attraction:
where S is the vector with magnitude (x^{2 }+ z^{2})^{1/2} from the origin to the particle projected on a plane perpendicular to the motion. In the xy plane, the particles move in epicycles as depicted in fig. 3.3.1.
If there is a large number of particles oscillating about their guiding centers, and if their oscillations are damped by mutual inelastic collisions or by the presence of a gas in the spacecraft, the eventual result will be that they all come to rest lined up along the y axis. (The particles may also reach equilibria when in contact with the walls of the spacecraft.)
6.4.2. Longitudinal Apparent Attraction
Suppose that a particle or grain of unit mass orbits in a circle with radius r_{0} around a central point mass M_{c}, and the motion is perturbed by the gravitational force
[90] of a small body m_{per} << M_{c} situated in the xy plane at a distance r_{per} from the origin of the moving coordinate system (xyz). It is assumed that this force is applied during a short time interval . It causes a change in the specific angular momentum C of a particle by The difference in the specific angular momenta of a particle at (0, y_{1}, 0) and a particle at the center of gravity of the spacecraft is given by
where
The new motion of the perturbed particle can be described as a circular motion of the guiding center modulated by a motion in an epicycle (fig. 6.4.1). The new orbital radius of the guiding center is Using
and defining the symbol , we have
Since the position of the particle is changed during the short interval t the x axis of the epicycle is equal to x_{0}, and consequently the y axis is equal to 2x_{0}. The particle moves in the retrograde direction in the epicycle, and the center of the epicycle moves in a circle with the angular velocity where, because = C/r^{2}= (GM_{c})^{2}/C^{3},
[91] Hence, after a time t the guiding center will be displaced in the y direction through a distance
in relation to an unperturbed particle.
To return to the problem discussed in sec. 6.4.1, we want to calculate how the linedup particles move in relation to the center of gravity of the spacecraft. Consider a particle situated at a distance y_{1} from the center of gravity of the spacecraft in the forward tangential direction. The velocity of its guiding center in relation to the center of gravity of the spacecraft is From eqs. (6.4.6) and (6.4.9), we find its displacement after a time t to be
Since , we can write
where
and
Further, we find from eq. (6.4.10),
Hence we see that the state of motion produced by the perturbation is such that the y values of all the guiding centers change in proportion to the original y value of the perturbed particle (fig. 6.4.1). We obtain A = 1 after a time t = t_{A=1}, which can be calculated from eq. (6.4.13). At this moment, all the guiding centers are on the same vector radius as the center of gravity of the spacecraft. The actual positions of the particles are scattered; however, all remain inside a square with its sides equal to 4x_{0} and its center at the center of gravity of the spacecraft.
A case of special interest occurs when
where n is an integer. If this relation is satisfied, all the particles are back at their initial position in the epicycle. Hence, all particles are simultaneously situated at the center of gravity of the spacecraft. The condition for this result is obtained from eqs. (6.4.13) and (6.4.15):
or
From the treatment of this idealized case we may conclude that, if the motion of the spacecraft is subject to perturbing gravitational fields satisfying certain conditions, the row of particles has a tendency to contract toward the center of gravity of the spacecraft. Hence, in addition to the transverse focusing discussed in sec. 6.4.1, there is also longitudinal focusing. Under certain conditions, which need to be investigated in detail, all the particles in the cabin are collected at one point (the center of gravity of the spacecraft). The condition for this to occur is expressed by eq. (6.4.18). In analogy with the transverse apparent attraction, the longitudinal [93] focusing may be considered to be the result of a longitudinal apparent attraction, although the type of motion produced by this attraction is rather different. Hence, we find that under certain conditions the center of gravity of the spacecraft "attracts" all the particles in the cabin, in the sense that the particles have a tendency to be brought together there. (If the perturbing force is directed along the x axis, there is instead an apparent repulsion by the center of gravity of the cabin.)
Because the spacecraft is assumed to have a negligible mass, one may ask why its center of gravity has such a remarkable property. The answer is that this point merely defines the state of motion of the whole assembly. Suppose that the mass of the spacecraft is much smaller than the mass of the particles and that their original common center of gravity was situated at an r larger than that of the spacecraft's center of gravity. Then the....
[94] ....particles would move more slowly than the spacecraft and would hit its backside wall, with the result that the spacecraft would be displaced outward so that its center of gravity would (almost) coincide with the center of gravity of the particles. (An exact statement would be possible only if the original state of motion of the particles were known.)
The apparent attraction is more important than the Newtonian attraction between two bodies of mass m_{1}, one of which is at the guiding center, if
which means that
For a spacecraft in orbit (r_{O}=10^{9} cm) around the Earth (M_{c} =6 X 10^{27} g), particles with a mass of 6 g must be much more than 1 cm apart for the apparent attraction to be more important than the gravitational attraction between the particles.
6.5. CONCLUSIONS FROM THE SPACECRAFT MODEL
We have treated a very simple model to clarify some aspects of celestial mechanics which are of special interest for studying accretional processes. The role of the spacecraft walls in our model is to compel all the particles to orbit with the same period. We have seen (sec. 6.4.1) that if the gravitational field is unperturbed (i.e., an inverse square force) the particles will align in the direction of motion along the line through the center of gravity of the spacecraft. If the orbits of the particles have nonzero eccentricities and/or inclinations, then their guiding centers will align along the path of the center of gravity of the spacecraft. This focusing, referred to as the transverse apparent attraction, is a consequence of the gravitational field of the central body around which the spacecraft orbits.
If the gravitational field is perturbed (sec. 6.4.2), we have found for certain types of perturbation that the particles move toward the center of gravity of the spacecraft. We have referred to this attraction as the longitudinal apparent attraction.
[95] It is important to consider to what extent similar phenomena may occur in astrophysics. Our model is based on the constraint that the particles all orbit with the same period. This effect can in reality he achieved by other means (for example, by gas friction, mutual collisions, and electromagnetic effects). The lining up of particles (due to transverse apparent attraction) is basically the same phenomenon as the focusing effects that produce jet streams in interplanetary space. The perturbationproduced attraction of the aligned particles to a common point (longitudinal apparent attraction) is related to the formation of bodies within jet streams, a process that is applicable to the formation of comets within meteor streams (ch. 14) In view of what has been said in sec. 6.1, we may look on our spacecraft as a jetstream workshop in which meteoroids are being produced (ch. 22).
6.6. JET STREAMS AND NEGATIVE DIFFUSION
Let us consider how mutual inelastic collisions can assume the role of the spacecraft walls in the model just discussed (i.e., to compel the particles to orbit with similar periods). Baxter and Thompson (1971) have treated the interaction between particles in Kepler orbits, considering the effect of inelastic collisions on the evolution of an initially smooth distribution of particle orbits. For a twodimensional system (all motion in a single plane), they found that inelastic collisions produced a negative diffusion coefficient. Hence, an initially smooth distribution will evolve and show radial density clustering (see fig. 6.6.1).
In a later paper, Baxter and Thompson (1973) generalized their results to a threedimensional case. They further concluded that, although in order to simplify the calculations they have assumed axisymmetry, this is not essential for the clustering. A similar process is expected to occur also in an eccentric jet stream.
These investigations are essentially an application of plasmaphysics formalism to the Kepler motion of grains, the grains assuming the role of interacting atoms, ions, and electrons in a plasma. This opens an interesting field of research that hopefully will lead to a better understanding of jet streams. For example, fragmentation and accretion at collision (which are not included in the simplified treatment by Baxter and Thompson) and the energy balance in a jet stream are important factors to be studied. Further, it is not yet clear what degree of inelasticity is required for jetstream formation Numerical simulations by Trulsen (1972b) have shown that, with elasticity exceeding a certain limit, jetstream formation does not take place.
Meteorites can yield much information on the processes occurring in their parent jet streams. Observations in meteorites demonstrate (secs. 22.6 [96] through 22.8) that most collisions involving their component grains were highly inelastic, leading to shock deformation, melting, and vaporization; solidified melt spray, broken rubble, and shocked metal are the most common components observed in ordinary chondrites and achondrites.
It should further be pointed out that collisions between the solid particles are not really necessary for jetstream formation. As is evident from the model of sec. 6.3, this can be achieved by a mechanism that makes the particles exchange momentum so that their orbital parameters become similar. As an example, suppose that all particles reemit gas molecules that have previously been temporarily incorporated by occlusion, implantation, or surface adsorption. The emitted molecules hit the other particles, thereby transferring momentum. The "viscosity" caused by the gas exchange may significantly contribute to jetstream formation. A theoretical investigation of this case is highly desirable; some discussion is given in sec. 6.8. The preservation of delicate features of condensed grains in carbonaceous meteorites provides suggestive observational evidence for equalization of orbital grain energy by means other than collision in these particular jet streams (sec. 22.6).
[97] 6.7. SIMPLE MODEL OF NEGATIVE DIFFUSION
We shall treat here a simple case that illustrates how the diffusion coefficient becomes negative. Consider a grain the guiding center of which orbits in a circle with radius r_{0} around a central body. The grain itself makes radial oscillations with amplitude x_{0} around the guiding center. Suppose that we have a population of such grains and divide it into two groups, one outside and one inside a certain value r'. For the first group, we define x_{1}_{ }= r_{1}_{ } r', and, for the second, x_{2} = r'r_{2} (see fig. 6.7.1). We suppose that x_{0}, x_{1}, and x_{2} are much smaller than r'.
Let all grains have the same mass and the same x,, and let all collisions between be perfectly inelastic. The number of collisions per unit time between grains in the intervals x_{1} to x_{1}_{ }+ dx_{1} with those in the interval x_{2} to x_{2}_{ }+ dx_{2} is
where N(x) is the number density of grains and a geometrical factor. As only if
collisions take place only inside the domain within the big triangle in fig. 6.7.1.
As the r value after collision between the two particles is
the result of a collision is a transfer of a guiding center outward through r' if x_{1}_{ }> x_{2}, and inward through r' if x_{2}_{ }> x_{1}. These domains of collisions are represented by the triangles a and b, respectively, in fig. 6.7.1. The net transport of guiding centers outward through r' is
[98] Suppose that the density varies linearly with r so that we may write
where N' is the number density at r' and is a constant. If is positive, the density increases outward; if is negative, the density decreases outward. We now have
Consider two equal surface elements, one in the triangle a and the other in b, situated symmetrically with respect to the border line x_{1}_{ }= x_{2}. For these two elements, x_{1}_{ }+ x_{2} and, hence, have the same value, but if > 0, the value of v is larger for the element in a than for the element in b (because x_{1}_{ }> x_{2}). The integrals in eq. (6.7.4) can now be evaluated by summing all such symmetric pairs of elements into which triangles a and b can be divided. Consequently, if > 0, D > 0. If < 0, we find D < 0, so that there is a net transport of guiding centers inward through r'.
Hence, we have shown that in either case an excess of guiding centers is transmitted from the lowdensity region into the highdensity region as a result of a collision. This means that the diffusion coefficient is negative.
6.8. CONTRACTION TIME OF A JET STREAM
Suppose that a body moves with velocity v_{0} and semimajor axis r_{0} in a Kepler orbit that is sufficiently close to a circle to allow us to treat it according to the guidingcenter method. Suppose further that the field is that due to an unperturbed inverse square force. Hence, the orbit of the body will remain an ellipse that does not precess.
Suppose this body emits a particle with velocity v (relative to the body) in the radial direction. This particle will oscillate with an amplitude
Similarly, particles emitted in the axial direction will oscillate with the same amplitude. Further, particles ejected in the tangential (forward) direction...
...will have the specific angular momentum C = r_{0} (v_{0}+v), which, because C = (GM_{c}r)^{1/2}, is the same as that for a particle orbiting in a circle of radius
if v << v_{0}. Hence, it will oscillate with the amplitude 2x_{0}, and its maximum distance from the orbit of the body will be 4x_{0}.
[100] The particles emitted with a velocity v will remain inside a torus with the small radius x = x_{0} where x_{0} is given by eq. (6.8.1) and is between 1 and 4, depending on the angle of emission. This result also applies to the case when the body does not move exactly in a circle.
If a body, or a number of bodies in the same orbit, emits gas molecules with a rms thermal velocity v = (3kT/m)^{1/2}, the gas will be confined within a torus with the typical thickness of
We will use x as a measure of the small radius of a jet stream even if some of the particles oscillate with a greater amplitude. As a typical example, the thermal velocity of hydrogen molecules at T = 300K is of the order 10^{5} cm/sec. If we put v_{0}_{ }= 3.10^{6} cm/sec (= the Earth's orbital velocity), we have, with = 1, x/ r_{0} = 1/30.
Jet streams differ from the rings in Laplacian theories in the respect that me mean free path of particles in a jet stream is long compared to the dimensions of the jet stream. Further, jet streams need not necessarily be circular. In fact, the phenomena we are discussing will take place even in jet streams with high eccentricity.
As no detailed theory of jet streams has yet been developed, we shall confine ourselves to an approximate treatment that gives at least a qualitative survey of some important phenomena. Suppose there is a jet stream consisting of a large number N of particles all confined to move inside a torus with small radius x. The average relative velocity between particles is u. If all particles have identical mass m and collisional cross section , each particle in the torus will collide with a frequency of the order
where t_{v} is the average time between two collisions and
is the number density. If each particle is a sphere with radius R and average [101] density , its mass is . The shape of the grains may deviate significantly from the spherical form (in the extreme case they may be needles), but for an orderofmagnitude estimate we assume a spherical shape. If we put the space density = mN we have
If we consider u = 1O^{5} cm/sec as a typical relative velocity and 3 g/cm^{3} as a typical grain density, we find for the respective values of grain radius R the values of given in table 6.8.1.
R 
= 
10^{3} 
1 
10^{3} 
10^{6} 
cm 

= 
4 x 10^{8} 
4 x 10^{5} 
4 x 10^{2} 
4 x 10^{+1} 
sec g cm^{3} 


1.3 x 10^{20} 
1.3 x 10^{17} 
1.3 x 10^{14} 
1.3 x 10^{11} 
g cm^{3} 
N 

1.1 x 10^{12} 
1.1 x 10^{18} 
1.1 x 10^{24} 
1.1 x 10^{30} 
cm^{3} 
To keep the jet stream together, the interval between collisions for a given particle t_{v} must be smaller than the time constant for the dispersive processes. Most important of these are the differential precession of the different orbits in the jet stream and the PoyntingRobertson effect. For an order of magnitude approximation we may put t_{v}_{ }=10^{5} yr = 3 x 10^{12} sec (see Whipple, 1968). This value for t_{v} gives the values of , and, from eq. (6.8.4), the values of N found in table 6.8.1.
The contraction of a jet stream is produced by inelastic collisions between the particles. The time constant for contraction should be a few times t_{v}. This also means that a jet stream can be formed only when there is no disruptive effect with a time constant less than t_{v}. For example, the differential precession of the pericenter and the nodes of an elliptic orbit will disrupt a jet stream unless t_{v} is smaller than the period of the differential precession.
A more refined model of jet streams should take into account the size distribution of the particles. Since the smallest particles are usually the most numerous, their mutual collisions will be the most efficient in keeping a jet stream together.
As the relative velocities in the interior of a jet stream decrease, the accretion of grains to form larger bodies will become more and more efficient. Hence to within an order of magnitude, t_{v} is the contraction time of the [102] jet stream. However, if larger bodies are formed, the result is that t_{v} will increase and the contractive force will be smaller. Eventually, the jet stream may no longer keep together.
It should be remembered that a jet stream is formed only if there is enough interaction between the particles. In the Saturnian rings, this interaction between the particles is very small. They do not form a jet stream but orbit with periods proportional to r^{3/2}.
6.9. COLLISIONS BETWEEN A GRAIN AND A JET STREAM
Let us examine what happens if a grain collides with a jet stream. Suppose that the grain moves in an orbit which at one point a crosses the jet stream (see fig. 6.9.1). (In principle, its orbit could cross the jet stream at four points, but we confine ourselves to the simplest case.) We are considering motions in an unperturbed Newtonian field, which means that me orbits remain unchanged unless the particles collide.
In the region where the grain crosses the jet stream, it will sooner or later collide with one of the particles of the stream. The collision is likely to be partially inelastic; in other words, part of the kinetic energy due to the relative motion is dissipated. The collision may result in breakup of one of the colliding grains, or of both, into a number of fragments.
After the collision, each of these fragments will move in a new orbit that in general differs from the initial orbit of the grains. This orbit may be situated either entirely within the jet stream or partially outside it. However, all possible orbits of the fragments will necessarily bring them back again to the point at which the collision took place. Since by definition this point was situated inside the jet stream, all the fragments will repeatedly cross the jet stream. (An exception to this rule occurs when the collision has taken place near the surface of the jet stream and the latter has had time to contract so much before the next collision that the point of the first collision then lies outside the stream.) Sooner or later this orbital intersection will lead to new collisions with the particles in the jet stream.
As on the average the collisions reduce the relative velocities, the fragments will finally be captured by the jet stream. At the same time, this capture will change the shape of the jet stream so that the new orbit is a compromise between its original orbit and the orbit of the colliding grain.
Hence, a grain that collides with a jet stream will be "eaten up" by it, with or without fragmentation. In the former case, the jet stream "chews" before it "swallows." This again can be considered as a consequence of the focusing effect of a Newtonian field.
In this way new kinetic energy is transferred to the jet stream, compensating for the decrease in its internal energy. If a large number of grains....
....are colliding with the jet stream, a temporary state of equilibrium is attained when the energy loss due to internal collisions is balanced by the energy brought in by the "eaten" particles. However, the new particles increase the value of N, and, hence, the energy loss. The final destiny in any case is a contraction of the jet stream (Ip and Mendis, 1974).
The internal structure of a jet stream depends on the size distribution and on the velocity distribution of its particles. We have only discussed the ideal case, in which all particles are identical. In a real jet stream, there is likely to be an assortment of bodies of all sizes subject to the competing processes of accretion and fragmentation. As the internal energy of the jet stream decreases, the relative velocities will also decrease. This means that collisions will not lead as often to fragmentation; accretion will dominate, and larger bodies will be formed inside the jet stream.
If the Newtonian field is perturbed, the jet stream will precess, the nodes moving in the retrograde sense and the pericenter moving in the prograde sense. However, the rate of precession depends on the orbital elements of me individual grains, and these are slightly different for each particle inside me jet stream. Hence, the perturbations tend to disrupt the jet stream. The permanence of the jet stream depends upon whether the viscosity, which keeps the jet stream together, is strong enough to dominate. In general, large bodies will leave the jet stream more readily than small bodies.
[104] 6.9.1. Conclusions
In accordance with what has been stated in sec. 1.1, we should not at present primarily aim at detailed theories but at a general framework in which such theories should be fitted. This describes the state of the jetstream discussion. Even if a detailed theory of jet streams is not yet developed, it seems legitimate to conclude as follows:
6.10. JET STREAMS AS CELESTIAL OBJECTS
The term "celestial object" includes planets, satellites, comets, stars, nebulae, galaxies, quasars, and pulsars. It would seem that jet streams should also be counted as "celestial objects." Certainly they are transient, but so are comets and nebulae.
The jetstream concept may be applied to several cases: