J002E3

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J002e3 animated.gif
J002E3 discovery images taken by Bill Yeung on September 3, 2002. J002E3 is in the circle.
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Computer simulation of J002E3's motion, alternating between six Earth orbits and a heliocentric orbit (click on image to view animation)
S-IVB stage of Apollo 17. The one used for Apollo 12 is of identical type. AS17-148-22714 crop.jpg
S-IVB stage of Apollo 17. The one used for Apollo 12 is of identical type.

J002E3 is an object in space which is thought to be the S-IVB third stage of the Apollo 12 Saturn V rocket. It was discovered on September 3, 2002, by amateur astronomer Bill Yeung. Initially thought to be an asteroid, it has since been tentatively identified as the third stage of Apollo 12 Saturn V based on spectrographic evidence consistent with the titanium dioxide in the paint used on the rockets. [1] [2] [3] The stage was intended to be injected into a permanent heliocentric orbit in November 1969, but is now believed instead to have gone into an unstable high Earth orbit which left Earth's proximity in 1971 and again in June 2003, with an approximately 40-year cycle between heliocentric and geocentric orbit. [4]

Contents

Discovery

When it was first discovered, it was quickly found that the object was in an orbit around Earth. Astronomers were surprised at this, as the Moon is the only large object in orbit around the Earth, [a] and anything else would have been ejected long ago due to perturbations with the Earth, the Moon and the Sun.

Therefore, it probably entered into Earth orbit very recently, yet there was no recently launched spacecraft that matched the orbit of J002E3. One explanation could have been that it was a 30 meter-wide piece of rock, but University of Arizona astronomers found that spectral observations of the object indicated a strong correlation of absorption features with a combination of human-made materials including white paint, black paint, and aluminum, consistent with Saturn V rockets. [2] Back-tracing its orbit showed that the object had been orbiting the Sun for 31 years and had last been in the vicinity of the Earth in 1971. This seemed to suggest that it was a part of the Apollo 14 mission, but NASA knew the whereabouts of all hardware used for that mission; the third stage, for instance, was deliberately crashed into the Moon for seismic studies.

The most likely explanation appears to be the S-IVB third stage for Apollo 12. [1] [2] Photometric observations of J002E3 made in February 2003 from the Air Force Maui Optical and Supercomputing Site (AMOS) matched an S-IVB light curve model consisting of a diffuse cylinder tumbling with a period of 63.46 seconds and a precession of 79 ± 10°. [5] NASA had originally planned to direct the S-IVB into a solar orbit, but an extra long burn of the ullage motors meant that venting the remaining propellant in the tank of the S-IVB did not give the rocket stage enough energy to escape the Earth–Moon system, and instead the stage ended up in a semi-stable orbit around the Earth after passing by the Moon on 18 November 1969.

It is thought that J002E3 left Earth orbit in June 2003, and that it may return to orbit the Earth in the mid-2040s. [1]

Potential impact with Earth or Moon

The object's Earth orbital paths occasionally take it within the radius of the Moon's orbit, and could result in eventual entry into Earth's atmosphere, or collision with the Moon. The Apollo 12 empty S-IVB, Instrument Unit, and spacecraft adapter base, had a mass of about 14 tonnes; 15 short tons (30,000 lb). [6] This is less than one-fifth of the 77.1-tonne; 85.0-short-ton (169,900 lb) mass of the Skylab space station, which was constructed from a similar S-IVB and fell out of orbit on 11 July 1979. [7] Objects with a mass of about 10 tonnes (22,000 lb; 11 short tons) enter Earth's atmosphere approximately 10 times a year, [8] one of which impacts the Earth's surface approximately once every 10 years. [9]

Ten essentially similar empty S-IVB stages from Apollo, Skylab and Apollo-Soyuz Test Project missions [b] have re-entered the atmosphere from 1966 to 1975. In all cases (including the Skylab station), the objects burned in the atmosphere and broke into relatively small pieces, rather than striking the Earth as a single mass. On the other hand, these objects entered from low Earth orbit or a ballistic trajectory, with less energy than J002E3 might possibly have if it were to enter from solar orbit.

See also

Notes

  1. ↑ Also orbiting the Earth are the Kordylewski clouds: large transient concentrations of dust at the Trojan points of the Earth–Moon system, discovered in 1956 by the Polish astronomer Kazimierz Kordylewski.
  2. ↑ The Apollo missions were: AS-201, AS-202, Apollo 4, Apollo 5, Apollo 6, and Apollo 7. The Skylab missions were Skylab 2, Skylab 3, and Skylab 4.

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References

  1. 1 2 3 Chodas, Paul; Chesley, Steve (11 October 2002). "J002E3: An Update". SpaceRef. NASA . Retrieved 25 August 2023.
  2. 1 2 3 Jorgensen, K.; Rivkin, A.; Binzel, R.; Whitely, R.; Hergenrother, C.; Chodas, P.; Chesley, S.; Vilas, F. (May 2003). "Observations of J002E3: Possible Discovery of an Apollo Rocket Body". Bulletin of the American Astronomical Society . 35: 981. Bibcode:2003DPS....35.3602J. Through the modeling of common spacecraft materials, the observations of J002E3 show a strong correlation of absorption features to a combination of human-made materials including white paint, black paint, and aluminum. Absorption features in the near IR show a strong correlation with paint containing a titanium-oxide semiconductor. Using the material model and the orbital information, it was concluded that J002E3 is a human-made object from an Apollo rocket upperstage, most likely Apollo 12.
  3. ↑ "First Confirmed Capture into Earth Orbit Is Likely Apollo Rocket". Jet Propulsion Laboratory. NASA. 20 September 2002. Archived from the original on 25 August 2023. Retrieved 25 August 2023.
  4. ↑ Chodas, Paul (11 September 2002). "Newly Discovered Object Could be a Leftover Apollo Rocket Stage". Center for Near Eath Object Studies. NASA. Archived from the original on 3 September 2018. Retrieved 25 August 2023.
  5. ↑ Lambert, John V.; Hamada, Kris; Hall, Doyle T.; Africano, John L.; Giffin, Maile; Luu, Kim Luu; Kervin, Paul; Jorgensen, Kira (2004). Photometric and spectral analysis of MPC object J002E3 . IEEE Aerospace Conference. Big Sky, Montana: IEEE. pp. 2866–2873. doi:10.1109/AERO.2004.1368093. OCLC   4801025397 . Retrieved 25 August 2023. … the rotational period was determined to be 63.46 seconds … The value determined for the precession angle, 79 ± 10°, indicates that the object is in a near end-over-end tumble … The optical cross-sections for the cylinder and the ends, 14 ± 2 and 5 ± 2 square meters, respectively, are consistent with the size of the S-IVB and the expected darkening of the white paint due to space weathering. Comparing the known physical dimensions of the S-IVB to the determined optical cross-sections yields an albedo for the cylinder of 0.16 ± 0.02 (neglecting the black painted areas) and 0.22 ± 0.07 for the ends.
  6. ↑ Orloff, Richard W. (September 2004). "Ground Ignition Weights". Apollo by the Numbers: A Statistical Reference.
  7. ↑ "Skylab Space Station". 6 June 2016.
  8. ↑ Bland, Philip (December 2005). "The impact rate on Earth". Philosophical Transactions of the Royal Society of London A . 363 (1837): 2793–2810. Bibcode:2005RSPTA.363.2793B. doi:10.1098/rsta.2005.1674. PMID   16286291. S2CID   19899735.
  9. ↑ Bland, Philip A.; Artemieva, Natalya A. (April 2006). "The rate of small impacts on Earth". Meteoritics . 41 (4): 607–631. Bibcode:2006M&PS...41..607B. doi: 10.1111/j.1945-5100.2006.tb00485.x . S2CID   54627116.
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