Luna 20

Last updated

References

  1. 1 2 Siddiqi, Asif (2018). Beyond Earth: A Chronicle of Deep Space Exploration, 1958–2016 (PDF) (second ed.). NASA History Program Office. ISBN   9781626830431.
  2. "Soviet and Russian Lunar Exploration" (PDF). p. 314.
  3. 1 2 "Table of Anthropogenic Impacts and Spacecraft on the Moon".
  4. "In Depth | Luna 20". NASA Solar System Exploration. Archived from the original on 2022-11-05. Retrieved 2020-02-05.
  5. "In Depth | Luna 20". NASA Solar System Exploration. 15 March 2018. Archived from the original on 2022-11-05. Retrieved 2020-02-05.
  6. Pillinger, Colin Trevor; Gowar, A.P (4 January 1977). "The separation and subdivision of two 0.5g samples of lunar soil collected by the Luna 16 and 20 missions" . Philosophical Transactions of the Royal Society of London. Series A, Mathematical and Physical Sciences. 284 (1319): 137–143. Bibcode:1977RSPTA.284..137P. doi:10.1098/rsta.1977.0003. S2CID   119730403.
  7. 1 2 3 "NASA – NSSDC – Spacecraft – Details". nssdc.gsfc.nasa.gov. Retrieved 2015-11-08.
  8. David, Leonard (18 March 2010). "NASA Lunar Orbiter Spots Old Soviet Moon Landers".
  9. "Luna-20 surface photos". Lunar Reconnaissance Orbiter Camera. Retrieved 2022-11-30.
Luna 20
Luna 20 descent stage.png
Luna 20 as seen from orbit by the LRO in 2010
Mission type Lunar sample return
OperatorSoviet space program
COSPAR ID 1972-007A OOjs UI icon edit-ltr-progressive.svg
SATCAT no. 5835
Mission duration11 days (day of launch to day of landing)
Spacecraft properties
Bus Ye-8-5
Manufacturer GSMZ Lavochkin
Launch mass5,725 kilograms (12,621 lb) [1]
Dry mass5,600 kilograms (12,300 lb)
Start of mission
Launch date14 February 1972, 03:27:58 (1972-02-14UTC03:27:58Z)  UTC [1]
Rocket Proton-K/D
Launch site Baikonur 81/24
End of mission
Landing date25 February 1972, 19:19 (1972-02-25UTC19:20Z) UTC
Landing site 47°24′N68°36′E / 47.400°N 68.600°E / 47.400; 68.600 , [2] 40 km north of Dzhezkazgan, Kazakhstan
Orbital parameters
Reference system Selenocentric
Semi-major axis 6,477.8 kilometres (4,025.1 mi)
Eccentricity 0.0
Periselene altitude 100 kilometres (62 mi)
Aposelene altitude 100 kilometres (62 mi)
Inclination 65 degrees
Period 119 minutes
Lunar orbiter
Orbits~36