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Figure 07-03 depicts the nine planets and moons to scale.
Table 07-01 below is a fact sheet about these planets and other planetary objects in ascending distance from the Sun, where Me = Mass of the Earth = 6x1027 gm. De = Diameter of the Earth = 1.3x109 cm. Distance from Sun to Earth = 1 AU = 1.5x1013 cm. Msun = 2x1033 gm. |
Figure 07-03 Planets |
Object | Mass (Me) | Size (De) | Distance (AU) | Rotation (Day) | Revolution (Year) | Satellite (#) | Surface Temp. (oC) | Density (H2O) | Atmospheric Composition |
---|---|---|---|---|---|---|---|---|---|
Sun | 3x105 | 100 | 0 | 25.38 | +5500 | 1.4 | H2 91%, He 9% | ||
Mercury | 0.06 | 0.38 | 0.39 | 58 | 0.24 | 0 | +350(day), -170(night) |
5.4 | Varies ~ O2 42%, N2 29%, H2 22% |
Venus | 0.95 | 0.95 | 0.72 | 243 | 0.62 | 0 | +475 | 5.3 | CO2 96%, N24% |
Earth | 1.00 | 1.00 | 1.00 | 1.00 | 1.00 | 1 | +22 | 5.5 | N2 78%, O2 21% |
Moon | 0.012 | 0.27 | 1.00 | 27.32 | 1.00 | +127 (day) -173 (night) |
3.3 | He, Ne, H2, Ar | |
Mars | 0.11 | 0.53 | 1.52 | 1.00 | 1.88 | 2 | -23 | 3.9 | CO2 95%,N2 3% |
Asteroid | < 10-4 | < .07 | ~ 2.7 | < 17 | 1 - 50 | 2.7 | |||
Jupiter | 318 | 11.2 | 5.20 | 0.4 | 11.86 | 16 | -123 | 1.3 | H2 90%, He 10% |
Saturn | 95 | 9.4 | 9.54 | 0.4 | 29.46 | >18 | -180 | 0.7 | H2 97%, He 3% |
Titan | 0.022 | 0.4 | 9.54 | 15.95 | 29.46 | -178 | 1.88 | N2 95%, CH4 5% | |
Uranus | 15 | 3.9 | 19.2 | 0.7 | 84.0 | >16 | -218 | 1.3 | H2 83%, He 15% |
Neptune | 17 | 3.8 | 30.1 | 0.7 | 164.8 | 8 | -228 | 1.6 | H2 79%, He 18% |
Pluto | 0.002 | 0.2 | 39.5 | 6.4 | 248 | 1 | -230 | 2.1 | N2 99.97%, CH4 |
UB313§ | 0.0025 | ~ 0.23 | ~ 97 | ~ -248 | |||||
Comet | ~ 10-12 | ~ 10-4 | 30 - 5x104 | 3 - 4x104 | 0.25 |
Name | Year | Cost | Mass (kg) | Comment |
---|---|---|---|---|
Apollo 11 | 1969 | 3 | 21.5 | First crewed Moon landing |
Apollo 12 | 1969 | 3.2 | 34.3 | Second mission to land humans on the Moon |
Apollo 14 | 1971 | 3.2 | 42.8 | Un-professional activity of playing golf on Moon |
Apollo 15 | 1971 | 3.7 | 76.8 | Longer stay and a greater focus on science |
Apollo 16 | 1972 | 3.7 | 95.3 | Focus on science, use of the Lunar Roving Vehicle |
Apollo 17 | 1972 | ~3.2 | 110.4 | Final mission of NASA's Apollo program |
Luna 16 | 1970 | ~ 0.2 | 0.1 | Uncrewed mission, part of the Luna programme |
Luna 20 | 1972 | ~ 0.2 | 0.05 | Another robotic competitor to the Apollos |
Luna 24 | 1976 | ~ 0.2 | 0.17 | Claiming detection of water ~ 0.1% by mass |
Hayabusa | 2003-2010 | ~ 0.105 | 0.000001 | Robotic spacecraft by Japan Aerospace Exploration Agency (JAXA) |
Hayabusa2 | 2014-2031 | ~ 0.27 | 0.0054 | Another asteroid sample-return mission operated by JAXA. |
OSIRIS-Rex | 2016-2029 | 1.16 | 0.25 | Sample collected from asteroid Bennu and delivered in 2023. Another sample collection will be from asteroid Apophis in 2029. |
Chang'e 5 | 2020 | 1.2 | 1.73 | First lunar sample-return mission since 1976, find water. Part of the "Chinese Lunar Exploration Program". |
Chang'e 6 | 2024 | ~ 1.2 | 2 | Samples from the far side of the Moon. See "September 21, 2024 Report", "November 15, 2024 Report" |
Mars Sample Return | 2020<2040 | < 11 | The project is too expensive, seeking new idea in 2024 |
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2. Regolith : o The regolith (lunar soil) consists of tiny rock fragments, glass beads, and dust, formed by the impact of micro-meteorites and solar wind weathering. o It includes particles of volcanic glass, indicating past volcanic activity on the Moon. |
Figure 07-04 Moon Rocks [view large image] |
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o The Chang'e 5 samples are expected to be among the youngest lunar rocks ever collected, with an estimated age of about 1.2 billion years. o This will help fill a significant gap in the lunar geological time line, providing insights into the Moon's volcanic activity during its later stages. 2. Volcanic Processes and History: o Detailed analysis of the basaltic rocks and volcanic glass in the samples will offer clues about the thermal and magmatic evolution of the Moon. o Understanding the composition and formation of these young volcanic rocks will shed light on the processes that continued to drive volcanic activity long after the Moon's major volcanic episodes had ended. |
Figure 07-05 Chang'e5 [view large image] |
See the Chinese language version : ![]() |
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o Mars Ascent Vehicle (MAV): The samples are loaded onto the MAV, which launches from the Martian surface into orbit around Mars. 6. Orbital Rendezvous and Transfer: o Orbiter Docking: The MAV docks with an orbiting spacecraft, transferring the sample container. o Orbit Transfer: The orbiting spacecraft adjusts its orbit for the return journey to Earth. 7. Return to Earth: o Earth Entry Vehicle: The spacecraft travels back to Earth, jettisoning a return capsule that enters Earth's atmosphere. o Re-entry and Landing: The return capsule re-enters Earth's atmosphere, decelerates using heat shields and parachutes, and lands safely for sample recovery. |
Figure 07-06 Mars Sample Return |
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3. OSIRIS-REx: o NASA's OSIRIS-REx mission, which collected samples from asteroid Bennu, also adheres to strict planetary protection measures. The samples are initially analyzed in highly controlled environments. |
Figure 07-07 Un-authorized Objects |