SP-345 Evolution of the Solar System

 

13. SPIN AND ACCRETION

 

[213] 13.1. GRAIN IMPACT AND SPIN

When an embryo grows by accreting grains, the spin of the embryo is determined by the angular momentum (in relation to the center of gravity of the embryo) which the grains transfer to the embryo. Suppose that a spherical embryo has a radius Rem, average density mathematical symbol
, and moment of inertia mathematical symbol, and that it is spinning with a period mathematical symbol
and angular velocity mathematical equation
. Its spin angular momentum is

 

mathematical equation(13.1.1)

 

We put

mathematical equation
(13.1.2)

 

where mathematical symbol
is the radius of gyration and mathematical symbol
the normalized radius of gyration. If the density of the spherical body is uniform, we have

 

mathematical equation
(13.1.3)

 

For celestial bodies with central mass concentration, mathematical symbol
is smaller (see table 2.1.1).

Suppose that a grain with mass mgn impinges with the velocity vimp on the embryo at an angle [Greek letter] psiwith the vertical. At impact, the spin angular momentum of the embryo changes by the amount

 

mathematical equation
(13.1.4)

[214] where Rem is the vector from the center of the embryo to the impact point. The absolute value of mathematical symbol
is

 

mathematical equation
(13.1.5)

 

Depending on the angle between mathematical symbol
and mathematical symbol
, the impact may increase or decrease the spin of the embryo.

We shall discuss the two-dimensional case where impacting particles orbit in the same plane as the embryo, and mathematical symbol
. is perpendicular to this plane. In this case mathematical symbol
is parallel to mathematical symbol
. We further assume mathematical symbol
<< mathematical symbol
. Then we have from eq. (13.1.1)

 

mathematical equation
(13.1.6)

 

Assuming that after the impact the accreted mass mgn will be uniformly distributed over the surface of the embryo (so that it keeps its spherical shape) we have

 

mathematical equation
(13.1.7)

and

 

mathematical equation
(13.1.8)

 

From eqs. (13.1.2) and (13.1.5 through 13.1.7) we find

 

mathematical equations
(13.1.9)

 

[215] or

 

mathematical equation
(13.1.10)

 

13.2. ACCRETION FROM CIRCULAR ORBITS BY NONGRAVITATING EMBRYO

The general problem of finding the spin of am accreting body is a very complicated many-body problem that is far from solved. Important progress has been made in the treatment of the two-dimensional problem when all the accreting grains are confined to move in the embryo's orbital plane. There is no obvious reason why a three-dimensional treatment (where the accreting grains move in orbits out of the embryo orbital plane) should not give the same qualitative results as the two-dimensional treatment, but this has not yet been checked by calculation. The conclusions we draw in the following sections are made with this reservation.

We shall start by treating the simple but unrealistic case where an assembly of grains moves in circular Kepler orbits (in an exact inverse r2 field or in the invariant plane of a perturbed field). We put the mass dm of the grains between the rings r and r + dr equal to mathematical equation
. A small embryo is orbiting in the circle r0 with a velocity mathematical equation
. The radius of the embryo is Rem its density is mathematical symbol (assumed to be uniform). We suppose that the accreted mass is immediately uniformly distributed over the surface of the embryo. (It should be observed that we assume the embryo to be a sphere but that the distribution of the grains is two-dimensional.)

As mathematical equation
is constant, a grain at the distance mathematical equation
. will have the angular velocity mathematical equation
. If mathematical symbol
<< r0 we have

 

mathematical equation
(13.2.1)

 

It will hit the embryo at the distance mathematical symbol
from the spin axis with the relative velocity

 

mathematical equation
(13.2.2)

 

If the mass of the grain is mgn, the angular momentum imparted to the embryo at impact is

[216] mathematical equation
(13.2.3)

 

As mathematical equation
we find that, when all the matter in the ring r0 - Rem to r0 + Rem is accreted, the embryo has the angular momentum

 

mathematical equation
(13.2.4)

 

and hence the spin velocity

mathematical equation
(13.2.5)

 

As the accreted mass is mathematical equation

 

 

mathematical equation
(13.2.6)

 

Hence the nongravitational accretion from circular grain orbits gives a slow retrograde rotation.

One would think that the case we have treated would be applicable at least to accretion by very small bodies. This is not the case for the following reason. It is possible to neglect the effect of gravitation on accretion only if

 

mathematical equation
(13.2.7)

 

where mathematical symbol
is the velocity of a grain at large distance and

 

mathematical equation
(13.2.8)

 

Substituting eqs. (13.2.2) and (13.2.8) into eq. (13.2.7) we have

 

[217] mathematical equation
(13.2.9)

 

or

 

mathematical equation
(13.2.10)

 

Even if [Greek letter] capital theta is as small as 1 g/cm3, we have [Greek letter] omega subscript 0>> 0.5 X 10-3 per sec, which is an unrealistic value.

 

13.3. GRAVITATIONAL ACCRETION

In the case of gravitational accretion1 by the embryo (see chs. 7 and 12), the velocity vimp of an impacting grain will equal or exceed the escape velocity ves of the embryo. In case the internal velocity or relative velocity within the jet stream is negligible, we have

 

mathematical equation
(13.3.1)

 

This is an important typical case which we shall discuss.

Equation (13.1.10) indicates how the spin of a spherical embryo (mathematical symbol
= 0.4) changes during accretion. If delta capital omega = 0 = 0 we have

 

mathematical equation
(13.3.2)

 

where we have introduced eq. (13.3.1) and put

 

 

mathematical equation
(13.3.3)

 

 

[218] Hence if the accretion occurs in such a way that sin [Greek letter] psi
, or rather the weighted mean of it, remains constant, and if we put

 

mathematical equation
(13.3.4)

where

mathematical equation
(13.3.5)

then the spin will tend toward the value

mathematical equation
(13.3.6)

 

This value is independent of Rem. If, however, after the accretion there is a density redistribution inside the body so that its relative radius of gyration changes from (0.4)1/2 to a value mathematical symbol , mathematical symbol
will change to

 

 

mathematical equation
(13.3.7)

 

Hence we see that this accretional model has a very important property: The spin of a body produced by planetesimal accretion is independent of the size of the body for a constant angle of incidence[Greek letter] psi
. A model with this property explains at least in a qualitative way the spin isochronism (see sec. 9.7); i.e., the remarkable fact that the spin of bodies of mass ranging from 1018 to 1030 g does not show any systematic dependence on the size of the body.

Spin isochronism lends empirical support for the type of planetesimal accretion theory we are discussing. It is also a strong argument against the idea of protoplanets with properties very different from the present planets, and it is impossible to reconcile spin isochronism with the hypothesis of planet and satellite origin by gravitational collapse of a precursor cloud.

The planetesimal model used above is too simplified to be applicable. We shall therefore discuss two other more realistic models which also account for the similarity of spins among accreted bodies.

 

[219] 13.4. GIULI'S THEORY OF ACCRETION

In order to find the numerical value of mathematical symbol
we must calculate Z. As stated above, we confine ourselves to a two-dimensional model. The problem is a many-body problem and can only be solved by using computers. This has been done by Giuli (1968a,b). He starts from the general planetesimal picture of accretion and assumes that the embryo of a planet (e.g., the Earth) orbits in a circle around the Sun. At the same time there is a uniform distribution of grains which when at large distance from the Earth....

 


FIGURE 13.4.1-Planetesimal orbits in a rotating coordinate system x,y, in Earth radii, centered on the Earth (according to Dole).

FIGURE 13.4.1-Planetesimal orbits in a rotating coordinate system x,y, in Earth radii, centered on the Earth (according to Dole). Small bodies (planetesimals) which originally move in circular orbits around the Sun with orbital radii greater than 1 AU will gradually be overtaken by the Earth. In a rotating coordinate system which fixes the Earth at the origin and the Sun on the abscissa to the left at a distance of 1 AU (thus assuming the Earth has a circular orbit), the particles will approach the Earth and will move in the complicated trajectories depicted in the figure. If their heliocentric orbital radii fall within seven ranges of values ("bands") all very close to the dashed line, they will hit the Earth. Otherwise, they will depart from the neighborhood of the Earth and return to heliocentric (but noncircular) orbits. Seven similar bands exist for particles with initial orbital radii less than 1 AU. (From Dole, 1962.)

 

[220] ....move in Kepler orbits around the Sun. When a grain comes into the neighborhood of the embryo, it is attracted gravitationally. If it hits the embryo, it is assumed to stick. The mass of the embryo will increase, and at the same time the grain transfers angular momentum to the embryo. The ratio between angular momentum and mass determines the spin of the embryo.

Dole (1962) has demonstrated that in order to hit an embryo moving in a circular orbit around the Sun the grains must be moving within certain "bands," defined in terms of their orbital elements. He calculates these for the case of grains which, before approaching the Earth, move in circular orbits around the Sun (see fig. 13.4.1). Giuli has made similar calculations which also include grains moving in eccentric orbits. (Like Dole, he restricts his calculations to the case of particles moving in the orbital plane of the embryo.) Further, he has calculated the spin which a growing planet acquires when it accumulates mass in this way.

He finds that a planet capturing exclusively those grains moving in circular orbits will acquire a retrograde rotation. However, if accretion takes place also from eccentric orbits, the rotation will be prograde (assuming equal grain density in the different orbits). This result is essentially due to a kind of resonance effect that makes accretion from certain eccentric orbits very efficient. In the case of the accreting Earth, such orbits are ellipses with semimajor axes a greater than 1 AU which at perihelion graze the planet's orbit in such a way that the grain moves with almost the same velocity as the Earth. There is also a class of orbits with a < 1 AU, the aphelion of which gives a similar effect. In both cases a sort of focusing occurs in such a way that the embryo receives a pronounced prograde spin.

Consider a coordinate system xy which has its origin at the center of the Earth. The Sun is at a great distance on the -x axis. The coordinate system rotates with the period of 1 yr. Using 1 AU as unit length and mathematical symbol
as time unit, the equations of motion for particles moving in Kepler orbits close to the Earth can be written approximately:

 

mathematical equation
(13.4.1)

mathematical equation
(13.4.2)

mathematical equation
(13.4.3)

mathematical equation
(13.4.4)

 


[
221]

FIGURE 13.4.2.-Particles shot out tangentially to the east with approximately the escape velocity from the point b on the Earth's equator (at 0600 hrs local time) will move in an ellipse with apogee at A.

FIGURE 13.4.2.-Particles shot out tangentially to the east with approximately the escape velocity from the point b on the Earth's equator (at 0600 hrs local time) will move in an ellipse with apogee at A. The motion is disturbed only minimally by the Coriolis force (2dy/dr) and by the tidal effect from the Sun (3x) because these forces are antiparallel. Particles shot out tangentially to the west under the same conditions experience parallel Coriolis and solar gravitational forces which deflect the trajectory from the elliptic orbit. (From Alfvén and Arrhenius, 1970b.)

 

The rotation of the coordinate system introduces the Coriolis force (2dy/dt), (2dx/dt) and the inhomogeneity of the solar gravitation, the force (3x, 0). These forces together disturb the ordinary Kepler motion around the planet. Capture is most efficient for particles moving through space with approximately the same speed as the Earth. These particles will hit the Earth at approximately the escape velocity ves. We can discuss their orbits under the combined gravitation of the Earth and the Sun in the following qualitative way. (See fig. 13.4.2.)

Let us reverse time and shoot out particles from the Earth. In case a particle is shot out from the 6-hr point of the Earth (x = 0, y =mathematical symbol
) in the eastward direction with slightly less than the escape velocity, it will move in an ellipse out in the -y direction toward its apogee A. The Coriolis force 2dy/dt and the solar gravitation gradient 3x will act in opposite directions so as to minimize the net disturbance. On the other hand, on a particle shot out in the westward direction from the 6-hr point the two forces will add in such a way as to deflect it from the ellipse far out from the Earth's gravitational field, where it will continue with a very low velocity.

Reversing the direction of motion we find that particles from outside can penetrate into the Earth's field in such a way that they hit the 6-hr point of the Earth's equator from the west but not from the east. Hence the particles form a sort of a jet which gives a prograde spin.

Similarly, particles moving inside the Earth's orbit can hit the 18-hr point only from the west, and they also give a prograde momentum.

Thus we have an efficient capture mechanism for two jets both giving prograde rotations (see fig. 13.4.3). They derive from particles moving in the solar field with about a = 1.04 AU and a = 0.96 AU and an eccentricity...

 


[
222]

FIGURE 13.4.3.-Planetesimals originally moving in slightly eccentric Kepler ellipses in the solar field may hit the Earth in two jets, both giving prograde rotation.

FIGURE 13.4.3.-Planetesimals originally moving in slightly eccentric Kepler ellipses in the solar field may hit the Earth in two jets, both giving prograde rotation.

 

....of 0.03. Most other particles hit in such a way that on the average they give a retrograde momentum.

Applied to the Earth, the net effect of the process is, according to Giuli, a prograde spin with a period of 15 hr, a value which is of the correct order of magnitude but larger by a factor of two or three than the Earth's spin period before the capture of the Moon (5 or 6 hr). Giuli finds that a body with the radius 0.1mathematical symbol
and the same density will acquire the same period. It is likely (although not proven mathematically) that the spin period is proportional to mathematical symbol
( [Greek letter] capital theta = density of me body, assumed to be homogeneous). The value of mathematical symbol
which is obtained in this way is

 

mathematical equation
(13.4.5)

 

This value is larger by a factor of about three than the average for all planets, including asteroids, which are not affected by tidal braking.

Giuli's calculations are based on the simplest possible planetesimal model, namely, that an embryo grows by accretion of those grains which hit it; collisions between the grains, for example, are not taken into account. It is highly satisfactory that this simple model gives the correct order of magnitude for the spin. It is reasonable to interpret this agreement as strong support for the theory of planetesimal accretion.

It should be mentioned that, if for some reason a planet accretes mainly from grains moving in orbits with small eccentricities, it should have a retrograde rotation. This means that if there is some reason to assume that Venus has accreted in this way, its retrograde rotation might be explained. We shall discuss this in sec. 13.6.3.

 

[223] 13.5. STATISTICAL THEORY OF ACCRETION

In Giuli's theory it is assumed

(1) That each planetesimal accreted by an embryo has a mass that is infinitely small compared to the mass of the embryo, and

(2) That planetesimals hit randomly.

There is no reason to doubt the second assumption, but whether the first one is correct depends on the type of accretion. As we have seen in ch. 12, mere are three different cases: Runaway accretion may be early, late, or delayed. We shall discuss these three cases in sec. 13.6.1.

 

13.5.1. Accretion Prior to Runaway Accretion

When planetesimals are accreting prior to runaway accretion their size distribution will no doubt be a continuous function, probably of the kind we find among the asteroids. The body we call the "embryo" is not fundamentally different from the other grains: it is primus inter pares. Hence, the largest planetesimals it is accreting are, although by definition smaller, not necessarily very much smaller than the embryo. If a planetesimal with a mass mathematical equation
, hits the embryo, one single planetesimal with a reasonably large [Greek letter] gamma can change the state of rotation drastically. Take as an extreme case that the planetesimal hits the embryo tangentially with the escape velocity. In fact it will give the embryo an additional angular velocity

 

mathematical equation
(13.5.1)

 

where

 

mathematical equation
(13.5.2)

 

and mathematical symbol
typically equals 0.33 (see table 2.1.1). The Giuli process gives to an order of magnitude Z = 0.1. In order to make Z' comparable we need only have mathematical equation
= 3 percent.

Hence, even one planetesimal with only a few percent of the mass of the embryo can under favorable conditions completely change the state of rotation of the embryo.

Levin and Safronov (1960), Safronov (1958 and 1960), and Safronov and Zvjagina (1969) on one hand, and Marcus (1967) on the other, have [224] considered the question of the relative sizes of bodies that collide randomly. Their results are not in quantitative agreement with each other, but they all show that statistical accretion should give a spin that on the average is of the same absolute magnitude as in Giuli's case, but directed at random.

Whereas an accretion from small grains (such as Giuli's mechanism) gives spin axes perpendicular to the orbital plane, the random accretion of large planetesimals gives a random distribution of spin axes. It is possible that this mechanism of statistical accretion is applicable to the spin of asteroids. However, for the small asteroids the escape velocity is very small and our models may meet difficulties because the approach velocities must be correspondingly small. It is possible that such low impact velocities are reconcilable with jet-stream accretion, but the problem no doubt needs further clarification.

 

13.6. JET-STREAM ACCRETION AND PLANETARY SPINS

We have found (ch. 12) that after exhaustion of the parent jet stream by runaway accretion an embryo accretes planetesimals that are very small. This means that the premises of Giuli's theory are applicable. Before and during the runaway phase, however, the embryo accretes planetesimals, some of which are of a size comparable to that of the embryo. Hence, a random spin vector due to the statistical arrival of large planetesimals is superimposed upon the spin vector which in the Giuli case is perpendicular to the orbital plane. The absolute value of the random vector is probably on the average about the same as the regular spin vector (see fig. 13.6.1).

 

13.6.1. Early, Late, and Delayed Runaway Accretion; Spin Inclination

Combining the above conclusions with the results on accretion in jet streams from ch. 12, we first discuss the cases involving an early runaway phase (Jupiter, Earth, Venus, and Mercury). Random spin is received by the growing embryo only before and during runaway accretion while it adds the first small part, typically 10 percent of its mass and 3 percent of its spin. Hence during most of the accretion the condition of infinitely small grains is satisfied, which means that the inclination of the equatorial plane towards the orbital plane should be small. This is indeed what is found for the case of the spin axis of Jupiter, the inclination of which is only 3°. Venus has a retrograde spin, for reasons that will be discussed in sec. 13.6.3, but the inclination of the axis of spin is only mathematical symbol
= 1° ( = 180° - 179°). In the case of the Earth, we should use the spin before the capture of the Moon.

[225] We do not know this value with certainty, but different theories for the evolution of the Earth-Moon system give low inclination values. Gerstenkorn (1969), for example, sets mathematical symbol
= 3O. The inclination of Mercury's spin may be influenced by its resonance capture.

The bodies which had a late runaway accretion (Saturn, Mars, and the Moon) have typically obtained 75 percent of their mass by accretion of a small number of bodies of relatively large size (statistical accretion). Only the last 25 percent of mass is accreted from small bodies (Giuli accretion). However, the Giuli accretion influences the spin more decisively because, due to the larger radius of the embryo, impacting planetesimals impart more spin angular momentum. Hence we would expect a superimposed random vector from statistical accretion of about one-half the regular vector from Giuli accretion. We find that both for Mars and for Saturn the spin axes inclinations are substantial (25° and 26°). We know nothing about the primeval spin of the Moon.

During a delayed accretion the entire process takes place by collision of large bodies (statistical accretion), so in this case we should have a large random spin vector. This applies to Uranus with mathematical symbol
= 98° and Neptune with mathematical symbol
= 29°, which indeed have the largest spin inclinations among all planets, although the difference between Neptune and Saturn is not large (see fig. 13.6.1).

 


FIGURE 13.6.1.

FIGURE 13.6.1. Spin vectors of the planets are represented by the light lines (length mathematical equation
). The Giuli-type accretion gives a vector bc equal to Jupiter's spin. The statistical accretion should give the vectors from c to the dots representing the different planets. Dashed lines represent "late runaway accretion," the heavy lines, "delayed runaway accretion."

 

[226] The number of planets we can apply our discussion to is only half a dozen. Our accretion mechanism involves a statistical element, but our sample is of course too small for any statistical analysis. However, we have found that the inclinations are smallest in cases where we should expect low values, and highest in the case of Uranus, where we should expect the random factor to dominate. This may be as far as it is possible to carry the analysis.

 

13.6.2. Spin Period

Concerning the absolute value of the spin vector the problem is less clear. In case embryos are accreting by the mechanism outlined in sec. 13.3, we should expect mathematical symbol to be constant. The model implies that the accreted body is homogeneous. If a differentiation takes place after the accretion, [Greek letter] tau should change as mathematical symbol
/0.4, so that the relevant quantity becomes mathematical symbol
. However, it is possible that the accreting embryo becomes inhomogeneous even at an early stage. Moreover the Giuli model is more complicated than the model of Sec. 13.3. Further, Giuli has only treated the two-dimensional case, and we have no theory for three-dimensional accretion. We should also observe that the conditions in a jet stream may be different from what has been assumed in the model of the theory of spin. This means that we must make much more sophisticated theoretical calculations before a quantitative comparison with observations can be made. We shall here confine ourselves to the following remarks:

(1) Assuming mathematical symbol
to have the same value for the primitive Earth as the present value for Jupiter, we find mathematical symbol
= 6 hr. This is higher than the Gerstenkorn value (sec. 13.6.1) but not in conflict with any observational data. It would speak in favor of a lunar capture in a polar or prograde orbit (see ch. 24).

(2) The period of Mars, which only by coincidence is similar to the period of the Earth today, is longer than expected by perhaps a factor of three. It may be futile to look for an explanation for this, other than the statistical character of the largest part of the Martian accretion history. In fact, accepting the Jovian accretion as normal for a nonrandom accretion, the vector from Jupiter to the other planets in fig. 13.6.1 should represent the random contribution. We see that the vector Jupiter-Mars is only about half the vector Jupiter-Uranus. In view of the fact that the entire Uranian accretion but only about half the Martian accretion is to be considered random, we have no reason to classify the slow Martian rotation as abnormal.

The same reasoning applies to the extremely slow rotation of Pluto (~6 days).

 

[227] 13.6.3. The Retrograde Rotation of Venus

As Giuli has shown, accretion exclusively from grains in circular orbits gives a retrograde spin, whereas, if grains in eccentric orbits are also accreted, the spin may become prograde. If we can show that the planetesimals from which Venus accreted moved in more circular orbits than the bodies from which the other planets accreted we may solve the problem of the anomalous rotation of Venus. A suggestion along these lines has recently been made by Ip (1974a).

 


1 The term gravitational secretion should not be confused with the gravitational instability of a gas cloud which, as shown in sec. 11.2, is not applicable to the formation of celestial bodies in the solar system, excepting the Sun.


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