Kosmos 382
| Mission type | Test Flight |
|---|---|
| Operator | Soviet Union |
| COSPAR ID | 1970-103A |
| SATCAT no. | 04786 |
| Mission duration | In Orbit: 53 years, 4 months and 23 days |
| Spacecraft properties | |
| Spacecraft type | Soyuz 7K-L1E |
| Start of mission | |
| Launch date | December 2, 1970, 17:00 UTC |
| Rocket | Proton K/D 8K82K |
| Contractor | Soviet Union |
| Orbital parameters | |
| Reference system | Low Earth Orbit |
| Inclination | 55.87° |
Kosmos 382 was a
Low Earth Orbit on a Proton rocket
designated as (Soyuz 7K-L1E No.2) on December 2, 1970.
The main purpose of the mission was to test the
Salyut space stations in the 1970s and 1980s.[2]
The following maneuvers were performed:
- 190 km x 300 km orbit to 303 km x 5038 km orbit (delta-V=982 meters/second;
- 318 km x 5040 km orbit to 1616 km x 5071 km orbit (deltaV= 285 m/s);
- 1616 km x 5071 km orbit to 2577 km x 5082 km orbit (deltaV= 1311 m/s).
See also
References
- ^ "Zond (L1E)". space.skyrocket.de.
- ^ "Публикации сотрудников АО "НИИхиммаш"" [Life Support Regeneration Systems for Long Space Flights (Publications by employees of JSC NIIhimmash)]. www.niichimmash.ru.
External links
| Launch vehicles and ascent/upper stages |  | |
|---|---|---|
| Spacecraft | ||
| Other hardware |
| |
docking tests | ||
| Zond (7K-L1/L1S) lunar flyby missions | ||
| LOK (7K-LOK/L1E) test missions |
| |
| LK Lander (T2K) test missions | ||
The † sign designates failed missions. Italics designates cancelled missions. | ||
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