File:1972_CPA_4113.jpg · Wikimedia Commons · See Wikimedia Commons
Key facts
- Mission type
- Mars orbiter/lander
- Operator
- Soviet space program
- Cospar id
- 1971-045A , 1971-045D
- Satcat number span no
- 5234, 5739
- Mission duration
- 1 year, 3 months and 3 days
- Spacecraft type
- 4M No. 171
- Manufacturer
- OKB-1
- Launch mass
- Total: , 4,650 kg (10,250 lb), Orbiter: , 3,440 kg (7,580 lb), Lander: , 1,210 kg (2,670 lb)
- Landing mass
- 358 kg (789 lb)
- Dry mass
- 2,265 kg (4,993 lb)
- Dimensions
- 4.1 × 2.0 × 5.9 m (13.5 × 6.6 × 19.4 ft)
- Launch date
- 19 May 1971, 16:22:44 ( 1971-05-19UTC16:22:44Z ) UTC
- Rocket
- Proton-K / D
- Launch site
- Baikonur 81/24
- Contractor
- Khrunichev
- Disposal
- Decommissioned
- Declared
- August 22, 1972 ( 1972-08-22 )
- Last contact
- July 1972
via Wikipedia infobox
Wikidata facts
Show 4 more facts
- UTC date of spacecraft launch
- 1971-05-19
- UTC date of spacecraft landing
- 1971-11-27
- service retirement
- 1972-08-22
- Commons category
- Mars 2
Sources (1)
via Wikidata · CC0
~8 min read
Article
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.