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Kosmos 382

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1970 Soviet test spaceflight
Kosmos 382
Soyuz 7K-L1E
Mission typeOrbital test flight
OperatorSoviet space program
COSPAR ID1970-103AEdit this at Wikidata
SATCATno.4786
Mission duration54 years, 11 months, 26 days (in orbit)
Spacecraft properties
Spacecraft typeSoyuz 7K-L1E
Start of mission
Launch dateDecember 2, 1970, 17:00 UTC
RocketProton-K/D
Launch siteBaikonur81/23
End of mission
DisposalDecommissioned
Last contactDecember 7, 1970
Orbital parameters
Reference systemGeocentric orbit
RegimeLow Earth Orbit
Perigee altitude2,577 km (1,601 mi)
Apogee altitude5,082 km (3,158 mi)
Inclination55.87°
← Zond 8

Kosmos 382 was aSovietSoyuz 7K-L1E modification of aSoyuz 7K-L1 "Zond" spacecraft and was successfully test launched intoLow Earth Orbit on aProton rocket designated as (Soyuz 7K-L1E No.2) on December 2, 1970.

The main purpose of the mission was to test theN1/L3 spacecraft'sBlock Dlunar orbit insertion/descent stage by simulating the lunar orbit insertion burn, the lunar orbit circularization burn and the final lunar descent burn. Over the course of five days, the Block D stage was ignited three times to raise the initial ~190 km × ~300 km × 51.6° orbit to a final 2577 km × 5082 km × 55.87° orbit. The Block D stage was fitted with cameras in the tanks to monitor the fuel and oxidizer behaviour in weightlessness and during acceleration.[1] Kosmos-382 also carried other experiments, including a prototype environmental control subsystem named "Rosa" for producing potable water from atmospheric condensate exhaled by cosmonauts onboard Soviet crewed spacecraft. This system was later used on theSalyut 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

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References

[edit]
  1. ^"Zond (L1E)".space.skyrocket.de.
  2. ^"Публикации сотрудников АО "НИИхиммаш"" [Life Support Regeneration Systems for Long Space Flights (Publications by employees of JSC NIIhimmash)].www.niichimmash.ru. Archived fromthe original on 2021-02-25. Retrieved2019-05-30.

External links

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Launch vehicles and
ascent/upper stages
LK spacecraft
Spacecraft
Other hardware
Soyuzdocking 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.
Payloads are separated by bullets ( · ), launches by pipes ( | ). Crewed flights are indicated inunderline. Uncatalogued launch failures are listed initalics. Payloads deployed from other spacecraft are denoted in (brackets).
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