Luna 16
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| Operator | Soviet Union |
|---|---|
| Major contractors | GSMZ Lavochkin |
| Mission type | Planetary Science Lunar Sample Return |
| Satellite of | Moon |
| Orbital insertion date | 17 September 1970 |
| Orbits | ~36 |
| Launch date | 12 September 1970 13:25:53 UTC |
| Carrier rocket | Proton 8K82K + Blok D |
| Launch site | Baikonur Cosmodrome |
| Mission duration | 12 days |
| Mission highlight | 101 gram sample returned to Earth |
| Landing | 24 September 1970 05:25 UTC |
| Landing site | 80 km (50 mi) SE of Dzhezkazgan, Kazakhstan |
| COSPAR ID | 1970-072A |
| Mass | 5,600 kg (12,000 lb) |
| Orbital elements | |
| Semimajor axis | 6,488.8 km (4,032.0 mi) |
| Eccentricity | 0 |
| Inclination | 70° |
| Apoapsis | 111 km (69 mi) |
| Periapsis | 111 km (69 mi) |
| Orbital period | 119 minutes |
| Moon landing | |
| Date | 20 September 1970 05:18 UTC |
| Coordinates | 0°41'S 56°18'E |
| Departure | 21 September 1970 07:43 UTC |
| Instruments | |
| Main instruments | Stereo photographic imaging system Remote arm for sample collection Radiation detector |
| References: NASA NSSDC Master Catalog | |
Luna 16 (Ye-8-5 series) was an unmanned space mission, part of the Soviet Luna program.
Luna 16 was the first robotic probe to land on the Moon and return a sample of lunar soil to Earth.[1] It represented the first lunar sample return mission by the Soviet Union, and was the third lunar sample return mission overall, following the Apollo 11 and Apollo 12 missions.
The spacecraft consisted of two attached stages, an ascent stage mounted on top of a descent stage. The descent stage was a cylindrical body with four protruding landing legs, fuel tanks, a landing radar, and a dual descent engine complex.
A main descent engine was used to slow the craft until it reached a cutoff point which was determined by the on-board computer based on altitude and velocity. After cutoff a bank of lower thrust jets was used for the final landing. The descent stage also acted as a launch pad for the ascent stage.
The ascent stage was a smaller cylinder with a rounded top. It carried a cylindrical hermetically sealed soil sample container inside a re-entry capsule.
The spacecraft descent stage was equipped with a television camera, radiation and temperature monitors, telecommunications equipment, and an extendable arm with a drilling rig for the collection of a lunar soil sample.
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Mission profile
The Luna 16 automatic station was launched toward the Moon from a preliminary Earth orbit and after one mid-course correction on 13 September it entered a circular 111 km with 70° inclination lunar orbit on 17 September 1970.
The lunar gravity was studied from this orbit. After two orbital adjustments were performed on 18 September and 19 September the perilune was decreased to 15.1 km, as well as the inclination altered in preparation for landing. At perilune at 05:12 UT on 20 September, the main braking engine was fired, initiating the descent to the lunar surface. Six minutes later at 05:18 UT, the spacecraft safely soft-landed in its target area at 0°41' south latitude and 56°18' east longitude, in the northeast area of the Mare Fecunditatis ("Sea of Fertility"), approximately 100 kilometers east of Webb crater. This was the first landing made in the lunar night side, as the Sun had set about 60 hours earlier. The main descent engine cut off at an altitude of 20 m and the landing jets cut off at 2 m height at a velocity less than 2.4 m/s, followed by vertical free-fall. The mass of the spacecraft at landing was 1,880 kilograms. Less than an hour after landing, at 06:03 UT, an automatic drill penetrated the lunar surface to collect a soil sample. After drilling for 7 minutes, the drill reached a stop at 35 centimeters depth and then withdrew its sample and lifted it in an arc to the top of the spacecraft, depositing the lunar material in a small spherical capsule mounted on the main spacecraft bus. The column of regolith in the drill tube was then transferred to the soil sample container.
Finally, after 26 hours and 25 minutes on the lunar surface at 07:43 UT on 21 September, the spacecraft's upper stage lifted off from the Moon. The lower stage of Luna 16 remained on the lunar surface and continued transmission of lunar temperature and radiation data. Three days later on 24 September, after a direct ascent traverse with no mid-course corrections, the capsule, with its 101 grams of lunar soil, reentered Earth's atmosphere at a velocity of 11 kilometers per second. The capsule parachuted down 80 kilometers southeast of the town of Jezkazgan in Kazakhstan at 05:25 UT on 24 September 1970. Analysis of the dark basalt material indicated a close resemblance to soil recovered by the American Apollo 12 mission.
According to the Bochum Observatory in the Federal Republic of Germany, strong and good quality television pictures were returned by the spacecraft.
Luna 16 was a landmark success for the Soviets in their deep space exploration program; the mission accomplished the first fully automatic recovery of soil samples from the surface of an extraterrestrial body.
- Launch Date/Time: 1970-09-12 at 13:25:53 UTC
- On-orbit dry mass: 5600 kg
Legacy
| Lunar Mission |
Sample Returned |
Year |
|---|---|---|
| Luna 16 | 101 g | 1970 |
| Luna 20 | 55 g | 1972 |
| Luna 24 | 170 g | 1976 |
Three tiny samples (.2 grams) of the Luna 16 soil were sold at Sotheby auction for $442,500 in 1993.[2] The samples are the only lunar rocks aside from Lunar meteorites and stolen rocks in private ownership during the 20th century.[2]
| Preceded by Luna 1970B |
Luna programme | Succeeded by Luna 17 |
References
- ^ Burrows, William E. (1999). This New Ocean: The Story of the First Space Age. Modern Library. pp. 432. ISBN 0375754857.
- ^ a b NY Times story, "F.B.I. Revisits Earthly Theft of Moon Rock
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