Luna 16 was an uncrewed space mission, part of the Soviet Luna program. It was the first robotic probe to land on the Moon and return a sample of lunar soil to Earth.[3][4] The 101 grams (3.56 ounces) sample was returned from Mare Fecunditatis. It represented the first successful lunar sample return mission by the Soviet Union and was the third lunar sample return mission overall.
![]() Luna 16 | |
Mission type | Lunar sample return |
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COSPAR ID | 1970-072A ![]() |
SATCAT no. | 4527 |
Mission duration | 12 days |
Spacecraft properties | |
Bus | Ye-8-5 |
Manufacturer | GSMZ Lavochkin |
Launch mass | 5,727 kg (12,626 lb) [1] |
Landing mass | 1,880 kg (4,140 lb) [1] |
Start of mission | |
Launch date | 12 September 1970, 13:25:53 (1970-09-12UTC13:25:53Z) UTC |
Rocket | Proton-K/D |
Launch site | Baikonur 81/23 |
End of mission | |
Landing date | 24 September 1970, 05:25 (1970-09-24UTC05:26Z) UTC |
Landing site | 47°24′N 68°36′E[2] |
Orbital parameters | |
Reference system | Selenocentric |
Semi-major axis | 6,488.8 km (4,032.0 mi) |
Eccentricity | 0 |
Periselene altitude | 111 km (69 mi) |
Aposelene altitude | 111 km (69 mi) |
Inclination | 70° |
Period | 119 minutes |
Epoch | 18 September 1970 |
Lunar orbiter | |
Orbital insertion | 17 September 1970 |
Orbits | ~36 |
Lunar lander | |
Landing date | 20 September 1970, 05:18 UTC |
Return launch | 21 September 1970, 07:43 UTC |
Landing site | 0.5137°S 56.3638°E / -0.5137; 56.3638 |
Sample mass | 101 grams (3.6 oz) |
Instruments | |
Stereo photographic imaging system Remote arm for sample collection Radiation detector | |
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.
The Luna 16 automated 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 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 UTC 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 Mare Fecunditatis (Sea of Fertility) approximately 100 kilometers west of Webb crater and 150 km north of Langrenus 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 seven 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.[1]
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.[1]
According to the Bochum Observatory in 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.
A 0.4825 g sample of material from a depth of 27 cm was sent to Britain.[5]
Lunar Mission |
Sample Returned |
Year |
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Luna 16 | 101 g (3.6 oz)[6] | 1970 |
Luna 20 | 30 g (1.1 oz)[7] | 1972 |
Luna 24 | 170 g (6.0 oz)[8] | 1976 |
Three tiny samples (0.2 grams) of the Luna 16 soil were sold at Sotheby's auction for $442,500 in 1993.[9] The samples were resold by Sotheby's for US$855,000 on 29 November 2018.[10]
A series of 10-kopeck stamps was issued in 1970 to commemorate the flight of Luna 16 lunar probe and depicted the main stages of the programme: soft landing on Moon, launch of the lunar soil sample return capsule, and parachute assisted landing back on Earth.
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← 1969 · Orbital launches in 1970 · 1971 → | |
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Kosmos 318 | OPS 6531 | Intelsat III F-6 | Kosmos 319 | Kosmos 320 | Kosmos 321 | Kosmos 322 | ITOS-1 · Australis-OSCAR 5 | DS-P1-I No.6 | SERT-2 | E-8-5 No.405 | Kosmos 323 | Ohsumi | OPS 0054 | Molniya-1 No.17 | Kosmos 324 | Kosmos 325 | OPS 0440 · OPS 3402 | Wika · Mika | Kosmos 326 | Meteor No.14 | Kosmos 327 | NATO 2A | Kosmos 328 | Kosmos 329 | Kosmos 330 | Nimbus 4 · Topo-1 | Kosmos 331 | OPS 7033 · OPS 7044 | Kosmos 332 | Apollo 13 | Kosmos 333 | OPS 2863 | Intelsat III F-7 | Kosmos 334 | Dong Fang Hong 1 | Kosmos 335 | Kosmos 336 · Kosmos 337 · Kosmos 338 · Kosmos 339 · Kosmos 340 · Kosmos 341 · Kosmos 342 · Kosmos 343 | Meteor No.13 | Kosmos 344 | Kosmos 345 | OPS 4720 · OPS 8520 | DS-P1-Yu No.36 | Soyuz 9 | Kosmos 346 | STV-3 | Kosmos 347 | Kosmos 348 | Kosmos 349 | OPS 5346 | Meteor-M No.17 | OPS 6820 | Molniya-1 No.21 | Kosmos 350 | Kosmos 351 | Unnamed | Kosmos 352 | Kosmos 353 | Zenit-4 No.75 | OPS 4324 | Intelsat III F-8 | Kosmos 354 | Interkosmos 3 | Kosmos 355 | Kosmos 356 | Venera 7 | OPS 7874 | Skynet 1B | Kosmos 357 | Kosmos 358 | Kosmos 359 · Kosmos 359 | OPS 8329 | Transit O-19 | Kosmos 360 | OPS 7329 | Orba · X-2 | OPS 0203 | Kosmos 361 | Luna 16 | Kosmos 362 | Kosmos 363 | Kosmos 364 | MS-F1 | Kosmos 365 | Molniya-1 No.19 | Kosmos 366 | Kosmos 367 | Kosmos 368 · Nauka No.3 | Kosmos 369 | Kosmos 370 | Kosmos 371 | Interkosmos 4 | Meteor-M No.16 | Kosmos 372 | Kosmos 373 | Zond 8 | Kosmos 374 | OPS 7568 | Kosmos 375 | Kosmos 376 | OPS 5960 | OFO · RM-1 | Luna 17 (Lunokhod 1) | Kosmos 377 | Kosmos 378 | OPS 4992 · OPS 6829 | Kosmos 379 | Kosmos 380 | Molniya-1 No.23 | OAO-B | Kosmos 381 | Kosmos 382 | Kosmos 383 | Kosmos 384 · Nauka No.2 | NOAA-1 · CEPI | Uhuru | Kosmos 385 | Peole | Kosmos 386 | Kosmos 387 | Kosmos 388 | Kosmos 389 | DS-P1-M No.1 | Molniya-1 No.22 | |
Payloads are separated by bullets ( · ), launches by pipes ( | ). Crewed flights are indicated in underline. Uncatalogued launch failures are listed in italics. Payloads deployed from other spacecraft are denoted in (brackets). |