Cosmos 382

Launch Success

Liftoff Time (GMT)

05:00:00 PM

Wednesday December 2, 1970

Mission Details

Launch Notes

Seven ignitions of the RD-58 engine were performed, all successfully.

Cosmos 382

Wiki

Cosmos 382 was a Soviet Soyuz 7K-L1E modification of a Soyuz 7K-L1 "Zond" spacecraft and was successfully test-launched into 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 N1/L3 spacecraft's Block D lunar 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. 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 manned spacecraft. This system was later used on the Salyut space stations in the 1970s and 1980s.

Trans Lunar Injection

1 Payload

10,380 kilograms

Rocket

Retired
Proton-K/Block D

Active 1967 to 1976

Khrunichev State Research and Production Space Center logo

Manufacturer

Khrunichev

Rocket

Height: 56.14m

Payload to Orbit

LEO: 18,900 kg

GTO: 9,000 kg

Liftoff Thrust

8,840 Kilonewtons

Fairing

Diameter: 3.9m

Height: 8.9m

Stages

4

Launch Site

Site 81/23

Baikonur Cosmodrome, Kazakhstan

Fastest Turnaround

11 days 23 hours

Stats

Proton-K


25th

Mission

6th

Mission of 1970

Khrunichev State Research and Production Space Center


538th

Mission

80th

Mission of 1970

1970


112th

Orbital launch attempt