Mars 2

Mars 2
Mission typeMars orbiter/lander
OperatorSoviet space program
COSPAR ID1971-045A
1971-045D
SATCAT no.5234
5739
Mission duration1 year, 3 months and 3 days
Spacecraft properties
Spacecraft type4M No. 171
ManufacturerOKB-1
Launch massTotal:
4,650 kg (10,250 lb)
Orbiter:
3,440 kg (7,580 lb)
Lander:
1,210 kg (2,670 lb)[1]
Landing mass358 kg (789 lb)
Dry mass2,265 kg (4,993 lb)
Dimensions4.1 × 2.0 × 5.9 m (13.5 × 6.6 × 19.4 ft)
Start of mission
Launch date19 May 1971, 16:22:44 (1971-05-19UTC16:22:44Z) UTC
RocketProton-K/D
Launch siteBaikonur 81/24
ContractorKhrunichev
End of mission
DisposalDecommissioned
DeclaredAugust 22, 1972 (1972-08-22)
Last contactJuly 1972[2]
Orbital parameters
Reference systemAreocentric[3]
Periareion altitude1,380 km (860 mi)
Apoareion altitude24,940 km (15,500 mi)
Inclination48.9°
Period18 hours
Mars orbiter
Orbital insertion27 November 1971
Orbits362
Mars impact (failed landing)
Impact date27 November 1971
Impact site45°S 47°E / 45°S 47°E / -45; 47 (Mars 2 Lander impact)

Mars 2 stamp

The Mars 2 was an uncrewed space probe of the Mars program, a series of uncrewed Mars landers and orbiters launched by the Soviet Union beginning 19 May 1971.

The Mars 2 and Mars 3 missions consisted of identical spacecraft, each with an orbiter and an attached lander. The orbiter is identical to the Venera 9 bus. The type of bus/orbiter is the 4MV. They were launched by a Proton-K heavy launch vehicle with a Blok D upper stage. The lander of Mars 2 became the first human-made object to reach the surface of Mars, although the landing system failed and the lander was lost.

  1. ^ "NASA - NSSDCA - Spacecraft - Details".
  2. ^ See Mars 3 article in https://solarsystem.nasa.gov/resources/1060/beyond-earth-a-chronicle-of-deep-space-exploration/
  3. ^ Mark Wade. "Mars M-71". Encyclopedia Astronautica. Retrieved 27 May 2024.

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