Pay attention to atmospheric features such as density, coloration and movement.
Yellow and orange coloration are largely due to sulfur compounds, although in Titan's case its coloration comes from a heavy hydrocarbon haze. Jupiter's ammonia content also affects its color, and can be seen in the greenish tints reflected from the night sides of the Galilean moons. Methane absorbs light in the red and yellow wavelengths, leading to Uranus' (with less methane) and Neptune's (with more methane) coloration.Also look closely for surface features which might give clues to past tectonic, volcanic (source), geyser or meteor activity. Distinguish between volcanic and meteor craters by looking for impact debris and ejecta (source) (some craters could be calderas). Look for volcanic rilles (trenches) (source), lava flows (source) and domes (source), as well as ridges and scarps (cliffs) formed by cooling and shrinking. Note the presence of liquids (source), dust or ice, and evidence of major collisions. What do these tell you about the surface history?
To get a feel for how difficult this business is, read this analysis of Europa.Here is a radar map of Venus, and one of Titan, to help you identify surface features. We also include one of Mars because our other image was chosen to highlight atmospheric and polar features.
This image shows the planets to scale:
(source), and this one shows some of the moons to scale:
(source). This image shows the orbits of the outer planets:
(source).
Have you ever seen the far side of the Moon? (source)
(View GOES 2/26/98 eclipse images (source).)Here is a panorama of the meteor crater near Winslow, AZ, and a movie of the Peekskill fireball (source).(View Cosmos DVD 4, episode 6, on Voyager at Europa.)
(View Cosmos DVD 3, episode 4, comet simulations, on the Tunguska Event.)
(View Solar System Animations from the Minor Planet Center.)
Some of the smallest constituents of the Solar System are dust particles.
Portfolio Exercise 4: Categorize each body in the list above as to the distinguishing feature(s) of its landscape: tectonic, volcanic, geyser or meteoric. You may have some bodies in which multiple features are present.For any characterization other than meteoric, find NASA images which support your categories; include them (with source references) in your portfolio. Annotate the pictures, circling and identifying the features which support your categorization.
Body Perihelion Aphelion Ang. Diam. @ Orbital Orbital Rotational Axial Tilt (AU) (AU) ca. (as) Period (Yrs) Inclination Period (Days) Sun 1918 2.2 * 108 25.38 7.25 Mercury 0.3075 0.4667 13.03 0.241 7 58.65 0 Venus 0.718 0.728 65.44 0.615 3.39 -243 177.3 Earth 0.983 1.017 1 5. * 10-5 0.9973 23.45 The Moon 0.00243 0.00271 1968 0.075 5.145 27.32 6.68 Mars 1.381 1.666 25.73 1.881 1.8 1.026 25.19 Phobos 6.175 * 10-5 6.363 * 10-5 0.1047 8.731 * 10-4 1 1.026 Deimos 1.567 * 10-4 1.569 * 10-4 0.05824 0.003456 1.8 1.026 Gaspra 0.2917 Ida 0.193 Jupiter 4.952 5.455 50.1 11.86 1.305 0.4135 3.12 Io 0.00281 0.002832 1.2761 0.004844 0.04 1.769 Europa 0.004445 0.004526 1.097 0.009723 0.47 3.551 Ganymede 0.007138 0.007167 1.846 0.01959 0.21 7.155 Callisto 0.0125 0.01268 1.684 0.04569 0.51 16.69 Saturn 9.021 10.05 20.76 29.4 2.484 0.444 26.73 Mimas 0.001215 0.001265 0.06753 0.00258 1.53 0.9424 Enceladus 0.001584 0.001598 0.0851 0.003751 0 1.37 Tethys 0.00197 0.00197 0.1826 0.005169 1.86 1.888 Dione 0.002517 0.002528 0.1929 0.007493 0.02 2.737 Rhea 0.00352 0.003527 0.2632 0.01237 0.35 4.518 Titan 0.007929 0.008406 0.8871 0.04366 0.33 15.95 Hyperion 0.00887 0.01093 0.03062 0.0583 0.43 13 (chaotic) Iaepetus 0.02313 0.02448 0.2474 0.2172 14.72 79.33 Uranus 18.29 20.1 4.086 84.02 0.77 -0.7196 97.86 Miranda 8.658 * 10-4 8.705 * 10-4 0.03769 0.00387 4.2 1.413 Ariel 0.001272 0.001281 0.09246 0.0069 0.3 2.52 Titania 0.00291 0.002923 0.126 0.02384 0.14 8.706 Neptune 29.81 30.33 2.372 164.8 1.769 0.6712 29.58 Triton 0.002371 0.002371 0.1295 -0.01609 157.3 -5.877 ("ca." stands for "closest approach".)
Since we telescopically measure only angular positions in the sky, we cannot measure perihelion and aphelion directly; we require an independent measurement of distance. This is done, for example, by radar ranging of Venus at closest approach. Thus the perihelion and aphelion values are actually computed and not directly observed. Planetary orbits are elliptical, and orbital parameters such as perihelion and aphelion are obtained by fitting careful measurements to elliptical orbits.
The data in the tables in this section come from NASA. There is an Excel spreadsheet available containing some of this information. It will serve as a starting point for your efforts to duplicate the conclusions below.
In this plot, the sum of the lengths of the two red lines is a constant for every point on the ellipse.Using the above information and the equations
and
we can compute the following parameters:
Of course, a and e are sufficient to describe any one of these orbits, but in order to understand how the planets are oriented with respect to each other we need 4 additional values:
Body a(AU) Eccentricity R(m) R(Earth) Sun 1.62 * 109 6.955 * 108 109 Mercury 0.3871 0.2056 2.44 * 106 0.3825 Venus 0.7233 0.0068 6.052 * 106 0.9488 Earth 1 0.01671 6.378 * 106 1 The Moon 0.00257 0.0549 1.734 * 106 0.2719 Mars 1.524 0.0934 3.397 * 106 0.5326 Phobos 6.269 * 10-5 0.015 1.3816 * 104 0.002166 Deimos 1.568 * 10-4 5. * 10-4 7688 0.001205 Gaspra 8428 0.001321 Ida 1.57 * 104 0.002462 Mathilde 2.971 * 104 0.004658 Jupiter 5.203 0.04839 7.149 * 107 11.21 Io 0.002821 0.004 1.821 * 106 0.2855 Europa 0.004485 0.009 1.565 * 106 0.2454 Ganymede 0.007153 0.002 2.634 * 106 0.413 Callisto 0.01259 0.007 2.403 * 106 0.3768 Saturn 9.537 0.05415 6.027 * 107 9.449 Mimas 0.00124 0.0202 1.96 * 105 0.03073 Enceladus 0.001591 0.00452 2.47 * 105 0.03873 Tethys 0.00197 0 5.3 * 105 0.0831 Dione 0.002523 0.00223 5.6 * 105 0.0878 Rhea 0.003523 0.001 7.64 * 105 0.1198 Titan 0.008167 0.02919 2.575 * 106 0.4037 Hyperion 0.0099 0.104 8.878 * 104 0.01392 Iaepetus 0.02381 0.02828 7.18 * 105 0.1126 Uranus 19.19 0.04717 2.559 * 107 4.012 Miranda 8.681 * 10-4 0.0027 2.36 * 105 0.037 Ariel 0.001276 0.0034 5.79 * 105 0.09078 Titania 0.002916 0.0022 7.889 * 105 0.1237 Neptune 30.07 0.00859 2.476 * 107 3.883 Triton 0.002371 1.6 * 10-5 1.352 * 106 0.212 Tempel 1 3103 4.865 * 10-4 Wild 2 2750 4.312 * 10-4 (Here and in the following, "(Earth)" means the values are multiples of that value for the Earth.)
Together these 6 values are called orbital elements. From them we can predict the past and future positions of any of the planets, to reasonable accuracy, within about 20 years of the time mentioned above. Beyond those dates, gravitational interactions between the planets must be taken into account.
There are subtle variations in eccentricity and tilt which cause long term cycles in the amount of sunlight received in the northern hemisphere, and which drive cyclic climate change:
These cycles were discovered by Milutin Milankovitch, a Serbian mathematician, and account for the ice ages which occur in 100000 and 41000 year cycles, as well as the smaller variations that occur in 19000 to 23000 year cycles (source).
They do not account for the increases in average global temperature since 1880.
Portfolio Exercise 5: Compute the following characteristics for each body in the table above: volume (in units of Earth's volume), surface area (in units of Earth's surface area) and average orbital velocity (in km/hour). Include details on the formulas used to compute the radius of each body.
orbital period = 2 * p * (semimajor axis3 / (G * mass))1/2we can compute the mass of any body with an orbiting satellite using the satellite's orbital parameters. But since we are able to send probe satellites to these bodies, we are able to measure their masses more accurately by measuring their gravitational influence on the paths of our probes and using Newton's Equation:
force due to gravity = G * mass1 * mass2 / distance2The relationship between Newton's Law of Gravity and Kepler's Laws of Motion is discussed in a Mathematica Notebook. You need Mathematica or Mathematica Player to view Mathematica Notebooks.Gauss' Law tells us that the gravitational force due to a spherically symmetric mass is equivalent to the force due to a point particle of the same mass, located at the center. Therefore we will usually treat planets (and stars!) as if all their mass was located at a point at their center.
Using these masses, we can compute a number of interesting parameters: their average densities,
their surface gravities (by setting
"mass2" to 1 and "distance" to the radius), their orbital angular momenta ("L", using the equation
Several densities of interest:
Planetary magnetic fields are believed to be the product of rotation and liquid metallic cores.
We have been able to measure the magnetic fields of some of these bodies using space probes:
(source),
Jupiter in x-ray wavelengths:
(source) and Saturn
in ultraviolet wavelengths:
(source). There is also a good
movie of terrestrial auroras from the POLAR mission
(source).
For each body in the table above, compute the orbital velocity at a distance of 400 km from the surface, and
the escape velocity from the surface. Compute each value in both km/hr and in multiples of the Earth's value.
It is also interesting to compare the tidal accelerations caused by some of these bodies on others. We will define the tidal
acceleration as the difference between the gravitational acceleration on the near side of the body and that at its center:
In addition, it is interesting to compare the tidal accelerations to that of Europa on Io, which is thought to account
for much of Io's internal heating, and subsequent active volcanism. Note that values in the final column are all less than 1.
If the tidal acceleration were equal to or greater than the surface gravity, the body would be gravitationally
unstable and would break up. This happens to bodies lying withing the Roche Limit.
Saturn's Rings lie within Saturn's Roche Limit:
In addition, for some of these bodies we have been
able to measure the surface temperature using space probes. Using these temperatures, we can learn something about
possible atmospheres. If the average molecular speed of a gas
(View GOES Isabel mov (source);
Saturn mov (source),
Cosmos DVD 4, episode 6, on Jupiter, the Red Spot and Neptune.)
angular momentum = 2 * p * mass * rotation rate * orbital radius2)
and their central pressures. The last we can estimate from dimensional considerations, using the formula
pressure = G * mass2 / radius4
Note that this value of the Earth's central pressure is 14.23 million times the atmospheric pressure on the surface.
Two other quantities worth noting are the orbital velocity (obtained from equating the gravitational acceleration to the
acceleration v2/r required to keep a body moving in a circular orbit):
Body M(kg) M(Earth) Density g(Earth) L (kgm2/s)
L(Earth) Central Pres. Central Pres. (g/cm3) (Pa) (Earth) Sun 1.989 * 1030 3.33 * 105 1.411 28 1.424 * 1056
5.349 * 1015 1.128 * 1015 784.1 Mercury 3.302 * 1023 0.05528 5.429 0.3778 9.149 * 1038
0.03437 2.054 * 1011 0.1427 Venus 4.868 * 1024 0.815 5.244 0.9053 1.846 * 1040
0.6934 1.179 * 1012 0.8195 Earth 5.974 * 1024 1 5.496 1 2.662 * 1040
1 1.439 * 1012 1 The Moon 7.348 * 1022 0.0123 3.365 0.1664 2.884 * 1034
1.083 * 10-6 3.986 * 1010 0.0277 Mars 6.418 * 1023 0.1074 3.909 0.3788 3.531 * 1039
0.1326 2.064 * 1011 0.1435 Phobos 1.063 * 1016 1.779 * 10-9 0.9623 3.792 * 10-4 2.132 * 1026
8.009 * 10-15 2.07 * 105 1.438 * 10-7 Deimos 2.38 * 1015 3.984 * 10-10 1.25 2.742 * 10-4 7.545 * 1025
2.835 * 10-15 1.082 * 105 7.52 * 10-8 Jupiter 1.899 * 1027 317.8 1.24 2.53 1.932 * 1043
725.8 9.209 * 1012 6.4 Io 8.932 * 1022 0.01495 3.531 0.1834 6.538 * 1035
2.456 * 10-5 4.841 * 1010 0.03364 Europa 4.8 * 1022 0.008035 2.989 0.1335 4.426 * 1035
1.663 * 10-5 2.563 * 1010 0.01781 Ganymede 1.482 * 1023 0.02481 1.936 0.1455 1.725 * 1036
6.479 * 10-5 3.044 * 1010 0.02116 Callisto 1.076 * 1023 0.01801 1.851 0.1269 1.662 * 1036
6.245 * 10-5 2.317 * 1010 0.0161 Saturn 5.685 * 1026 95.17 0.62 1.066 7.837 * 1042
294.4 1.635 * 1012 1.136 Mimas 3.75 * 1019 6.278 * 10-6 1.189 0.006648 9.96 * 1031
3.742 * 10-9 6.359 * 107 4.419 * 10-5 Enceladus 7. * 1019 1.172 * 10-5 1.109 0.007814 2.105 * 1032
7.907 * 10-9 8.785 * 107 6.105 * 10-5 Tethys 6.27 * 1020 1.05 * 10-4 1.005 0.0152 2.097 * 1033
7.879 * 10-8 3.325 * 108 2.311 * 10-4 Dione 1.1 * 1021 1.841 * 10-4 1.495 0.02389 4.163 * 1033
1.564 * 10-7 8.21 * 108 5.706 * 10-4 Rhea 2.31 * 1021 3.867 * 10-4 1.237 0.02695 1.033 * 1034
3.881 * 10-7 1.045 * 109 7.263 * 10-4 Titan 1.346 * 1023 0.02252 1.881 0.1382 9.161 * 1035
3.442 * 10-5 2.748 * 1010 0.0191 Hyperion 8 * 1017 1.339 * 10-7 0.2729 6.912 * 10-4 5.993 * 1030
2.251 * 10-10 6.875 * 105 4.778 * 10-7 Iaepetus 1.6 * 1021 2.678 * 10-4 1.032 0.02114 1.86 * 1034
6.989 * 10-7 6.428 * 108 4.467 * 10-4 Uranus 8.685 * 1025 14.54 1.237 0.9032 1.696 * 1042
63.73 1.174 * 1012 0.8157 Miranda 6.6 * 1019 1.105 * 10-5 1.199 0.00807 5.728 * 1031
2.152 * 10-9 9.371 * 107 6.512 * 10-5 Ariel 1.35 * 1021 2.26 * 10-4 1.66 0.02742 1.42 * 1033
5.336 * 10-8 1.082 * 109 7.52 * 10-4 Titania 3.53 * 1021 5.909 * 10-4 1.716 0.03863 5.613 * 1033
2.109 * 10-7 2.147 * 109 0.001492 Neptune 1.024 * 1026 17.15 1.61 1.138 2.505 * 1042
94.09 1.862 * 1012 1.294 Triton 2.14 * 1022 0.003582 2.067 0.07973 -3.333 * 1034
-1.252 * 10-6 9.146 * 109 0.006356
orbital velocity = (G * mass / distance)1/2
and the escape velocity (obtained from equating the kinetic energy mv2/2 to the gravitational energy Gm/r):
escape velocity = (2 * G * mass / distance)1/2
In both of these equations, the mass is the mass of the body we are orbiting or escaping from; the results are independent
of the mass of our spacecraft. The distance in each equation is the distance from the center of the body (its radius in the case of the escape velocity).
Here are images of auroras on Earth in optical wavelengths:
Body Magnetic Field (Earth) Sun 2 Mercury 0.011 Venus 0.001 Earth 1 Mars 0.001 Jupiter 13.89 Saturn 0.67 Uranus 0.74 Neptune 0.43
Portfolio Exercise 6:
Use the relation between the orbital period, the semimajor axis length and the total mass, to compute the masses of the Sun and
those planets with moons.
Recall from our derivation of Kepler's Laws from Newton's that the mass in this relation is the combined mass of the parent
and the satellite. For this reason, you will get the best results if you choose the satellite with the lowest mass (ie., use
Mercury's orbital parameters to compute the mass of the Sun, Deimos' to compute Mars' mass, etc.).
Compare these values to the measured values quoted above: in terms of a percentage, how far off
are your values from those in the table above?
Gravity and Tides
Using the masses above, it is interesting to compare the strengths of the gravitational forces among some of these bodies.
This table gives the gravitational force between some of the planets and their moons, expressed as a fraction of the
gravitational force between the Sun and that planet:
We can see that many of the moons have a significant perturbative influence on the orbital motion of their planets.
Planet Body Fgrav (Sun) Earth The Moon 0.005594 Jupiter Io 0.1528 Jupiter Europa 0.03248 Jupiter Ganymede 0.03943 Jupiter Callisto 0.009244 Saturn Jupiter 0.004623 Saturn Tethys 0.00739 Saturn Dione 0.007904 Saturn Rhea 0.008511 Saturn Titan 0.09224 Uranus Miranda 0.01622 Uranus Ariel 0.1534 Uranus Titania 0.07685 Neptune Triton 1.73
accelerationtidal = G * mass1 * (1 / (distance - radius2)2 - 1 / distance2)
where the distance is the distance between the bodies, and the subscripts refer to their labels below. These values have
been expressed as fractions of the tidal acceleration of the Moon on the Earth (1.286 * 10-6 m/s2),
and as fractions of the body's own surface gravity.
Here are some time lapse photos of tidal phenomena caused by the Moon.
In all cases, the length of the orbital semimajor axis has been used to compute the distance:
All of the moons in this table are locked in synchronous orbits: their rotational period is equal
to their orbital period. This is due to tidal deformations (bulges toward the planet) which hold the same face
toward the planet at all times. Mercury is also in a sychronous orbit, but in a more complicated fashion because of its higher
eccentricity: it rotates 3 times for every 2 orbits around the Sun.
Body 1 Body 2 atidal (Moon on Earth) atidal / g Sun Mercury 2.955 9.008 * 10-7 Sun Venus 1.123 1.429 * 10-7 Sun Earth 0.4481 5.161 * 10-8 Sun The Moon 0.1218 8.43 * 10-8 Earth The Moon 21.7 1.502 * 10-5 The Moon Earth 1 1.152 * 10-7 Mars Phobos 1274 0.387 Mars Deimos 45.22 0.01899 Jupiter Io 5476 0.003438 Jupiter Europa 1167 0.001007 Jupiter Ganymede 484.5 3.837 * 10-4 Jupiter Callisto 80.96 7.349 * 10-5 Io Jupiter 13.33 6.069 * 10-7 Io Europa 1.081 9.327 * 10-7 Io Ganymede 0.1029 8.146 * 10-8 Europa Jupiter 1.593 7.252 * 10-8 Europa Io 0.6768 4.25 * 10-7 Europa Ganymede 0.2377 1.882 * 10-7 Ganymede Jupiter 1.135 5.168 * 10-8 Ganymede Io 0.1178 7.395 * 10-8 Ganymede Europa 0.4343 3.748 * 10-7 Callisto Jupiter 0.1444 6.574 * 10-9 Saturn Mimas 2067 0.03581 Saturn Enceladus 1233 0.01818 Saturn Tethys 1396 0.01058 Saturn Dione 701.9 0.003384 Saturn Rhea 351.6 0.001503 Saturn Titan 95.2 7.935 * 10-5 Saturn Hyperion 1.837 3.062 * 10-4 Saturn Iaepetus 1.069 5.825 * 10-6 Tethys Saturn 0.2478 2.677 * 10-8 Tethys Enceladus 0.1015 1.496 * 10-6 Dione Saturn 0.19 2.053 * 10-8 Dione Tethys 0.1229 9.31 * 10-7 Rhea Saturn 0.1352 1.461 * 10-8 Titan Saturn 0.5673 6.13 * 10-8 Titan Hyperion 0.08113 1.352 * 10-5 Uranus Miranda 1109 0.01583 Uranus Ariel 858 0.003604 Uranus Titania 97.81 2.917 * 10-4 Miranda Uranus 0.1275 1.626 * 10-8 Ariel Uranus 0.73 9.309 * 10-8 Ariel Miranda 0.1663 2.374 * 10-6 Titania Uranus 0.1409 1.797 * 10-8 Neptune Triton 368.9 5.33 * 10-4 Triton Neptune 1.565 1.585 * 10-7
(source)
In this image, green hues indicate particle sizes less than 5 cm, while blue indicates less than 1 cm. Purple regions had pieces larger than 5 cm
(up to several meters), and white indicates an area so dense that it was opaque to the radio waves used to probe the particle sizes.
Temperature and Atmosphere
By measuring the wavelength of maximum power output and using Wien's Law
wavelength of maximum thermal outputAngstroms = 2.9 * 107 Angstroms / temperature
we can measure the effective (black body) temperature of many of these bodies. Using Stefan's Law
power emitted or absorbed per unit area = 5.67 * 10-8 * temperature4
and the fact that power per unit area (intensity) decreases with the square of the distance, we can compare the
intensity of the radiation they receive to that which Earth receives (1365 W/m2), and the ratio of their output to input intensity
(for moons, we include the input both from the Sun and from their host planet).
average molecular speed = 157 * (temperature / molecular weightH = 1)1/2
is less than 1/6 of the planet's escape velocity at the surface
escape velocity = (2 * G * mass / radius)1/2
there is a high probability that the gas still exists in an atmosphere near the surface. We can use these two equations to
find the minimum molecular weight of any atmosphere for these bodies (the majority atmospheric component has been
provided for comparison purposes, when known):
Some possible atmospheric components of interest are:
Body Teff ISun (Earth) Iout/Iin Max Tsurface
Min Mol. Wt. Major Atmos. Comp. Surface Atmos. Pressure (Earth) Sun 5777 0 H Mercury 533 6.674 1.005 700 34 2 * 10-12 Venus 227 1.911 0.2308 735 6 C O2 90 Earth 255 1 0.7025 331 2 N2 1 The Moon 387 1 3.727 396 62 1 * 10-12 Mars 217 0.4308 0.8553 268 9 C O2 .006 Jupiter 125 0.03694 1.098 0 H2 Io 128 0.03694 1.198 17 Europa 128 0.03694 1.204 27 10-7 Ganymede 128 0.03694 1.206 15 Callisto 128 0.03694 1.207 19 Saturn 95 0.0101 1.231 0 H2 Titan 85 0.0101 0.7883 94 11 N2 1.6 Uranus 57 0.002715 0.646 0 H2 Miranda 86 0.002715 3.327 2044 Ariel 84 0.002715 3.038 239 Neptune 59 0.001106 1.82 0 H2 Triton 38 0.001106 0.3126 15 N2 1.4 * 10-5
After viewing these large-scale weather patterns on various planets, it is interesting to observe something
much smaller on Earth, and on Mars:
Atom or Molecule Molecular Weight H2 2 He 4 C H4 (methane) 16 N H3 (ammonia) 17 H2 O 18 C O 28 N2 28 C2 H6 (ethane) 30 O2 32 Ar 40 C O2 44 C3 H8 (propane) 44
(View Martian Dust Devils as photographed by Spirit (source))Compare two dust storms, one on Earth off the northwest coast of Africa, and one on Mars in the north polar regions (source):
Dust is responsible for heat transport on Mars much as water is here on Earth.
Gravity Waves are seldom noticed in action because of their long periods; this movie is a time lapse over 40 minutes:
(View movie of gravity wave (source))
AU Microscopii is a red dwarf star approximately 12 million years old with a debris disc; the radius of the cleared central region is approximately 7 AU:
Material Melting Point (K) Iron 1808 Silicon 1684 Ice 273 Ammonia 195 Methane 91
(source)
HD 107146 is a yellow star much like our Sun but between 30 and 250 million years old. The radius of the cleared central region is approximately 40 AU:
(source)
In comparison, the Kuiper Belt (home to short period comets) extends to about 50 AU from the Sun. The Oort Cloud (home to long period comets) has a radius of approximately 100000 AU.
The mass of Comet Halley is about 1014 kg. It is about 40% water and about 20% organic compounds. Assuming that it is an average comet, and that comets were responsible for the presence of water on the Earth, we can compute the frequency of cometary impact in the Earth's early history. These impacts occurred mainly during a period of about 200 million years, approximately 4 billion years ago. If the total amount of water on the Earth is 1.65 * 1021 kg, it would have taken 41.25 million cometary impacts, or an average of about 5 impacts a year. These impacts would have deposited a further 8.25 * 1020 kg of organic material.Here is a Hubble animation revealing a protoplanetary disc in the Orion Nebula (source). Note that during formation, accretion and fragmentation are both occurring, as well as frequent collisions.
(View Animations of Solar System Formation (source) (source))
©2008, Kenneth R. Koehler. All Rights Reserved. This document may be freely reproduced provided that this copyright notice is included.
Please send comments or suggestions to the author.