| Mission type | Venus flyby |
|---|---|
| Operator | OKB-1 |
| Harvard designation | 1962 Alpha Phi 1 |
| COSPAR ID | 1962-045A |
| SATCATno. | 389 |
| Mission duration | Launch failure |
| Spacecraft properties | |
| Spacecraft type | 2MV-2 |
| Manufacturer | OKB-1 |
| Launch mass | 6,500 kilograms (14,300 lb) |
| Start of mission | |
| Launch date | 12 September 1962, 00:59:13 (1962-09-12UTC00:59:13Z) UTC |
| Rocket | Molniya 8K78s/n T103-14 |
| Launch site | Baikonur1/5 |
| End of mission | |
| Decay date | 14 September 1962 (1962-09-15) |
| Orbital parameters | |
| Reference system | Geocentric |
| Regime | Low Earth (achieved) Heliocentric (intended) |
| Semi-major axis | 6,550 kilometres (4,070 mi) |
| Eccentricity | 0.02977 |
| Perigee altitude | 163 kilometres (101 mi) |
| Apogee altitude | 195 kilometres (121 mi) |
| Inclination | 64.8 degrees |
| Period | 88.07 minutes |
| Epoch | 1962-09-11, 21:40:00 UTC[1] |
Venera 2MV-2 No.1,[2][3] also known asSputnik 21 in the West, was aSoviet spacecraft, which was launched in 1962 as part of theVenera programme, and was intended to make aflyby ofVenus.[4] Due to a problem with the rocket which launched it, it failed to leavelow Earth orbit, and reentered the atmosphere a few days later.[5] It was the second Venera 2MV-2 spacecraft, both of which failed to leave Earth orbit.[3]
Venera 2MV-2 No.1 was launched at 00:59:13 UTC on 12 September 1962, atop aMolniya 8K78 carrier rocket flying fromSite 1/5 at theBaikonur Cosmodrome.[2] The rocket performed nominally until cutoff of theBlok I stage, following injection into alow Earth orbit. Following cutoff, one of the oxidiser valves failed to close, andliquid oxygen was allowed to flow into the combustion chamber of one of thevernier thrusters. The vernier thruster exploded,[6] causing the rocket to tumble out of control. This led to the formation of bubbles in the upper stage oxidiser pump, which caused the upper stage engine to fail less than a second after ignition.[3] It reentered the atmosphere on 14 September 1962, two days after it had been launched.[7]
The designations Sputnik 25, and later Sputnik 21, were used by the United StatesNaval Space Command to identify the spacecraft in its Satellite Situation Summary documents, since the Soviet Union did not release the internal designations of its spacecraft at that time, and had not assigned it an official name due to its failure to departgeocentric orbit.[4][8][1]
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