Kosmos 1001 | |
Mission Type: | Orbital test flight |
Operator: | Soviet space program |
Cospar Id: | 1978-036A |
Satcat: | 10783 |
Spacecraft: | Soyuz-T s/n 4L |
Spacecraft Type: | Soyuz 7K-ST (11F732) |
Manufacturer: | NPO Energia |
Launch Mass: | 6680kg (14,730lb) |
Launch Date: | GMT |
Launch Rocket: | Soyuz-U |
Launch Site: | Baikonur 1/5 |
Disposal Type: | Deorbited |
Landing Date: | GMT |
Orbit Reference: | Geocentric |
Orbit Periapsis: | 1990NaN0 |
Orbit Apoapsis: | 2280NaN0 |
Orbit Inclination: | 51.6° |
Orbit Period: | 88.7 min |
Apsis: | gee |
Programme: | Soyuz programme |
Previous Mission: | Soyuz 28 |
Next Mission: | Soyuz 29 |
Programme2: | Kosmos (satellites) |
Previous Mission2: | Kosmos 1000 |
Next Mission2: | Kosmos 1002 |
Kosmos 1001 (Russian: Космос 1001 meaning Cosmos 1001) was a redesigned Soviet Soyuz T spacecraft that was flown on an unmanned test in 1978. The spacecraft was the upgraded Soyuz for Salyut 6 and Salyut 7. This Kosmos flight, launched from Baikonur, was the first orbital flight of the Soyuz T design. Several maneuvers were tested, however it failed to achieve all of its objectives and resulted in an early deorbit and landing