Cosmos 57

Launch Success

Liftoff Time (GMT)

07:30:00

Monday February 22, 1965

Mission Details

Launch Notes

Uncrewed flight of the Voskhod spacecraft.

Cosmos 57

The Voskhod-3KD Cosmos 57 was a Soviet uncrewed spacecraft modified from the Voskhod-3KV and closely based on the Vostok-3K capsule. It was capable to carry crews of two cosmonauts and enabled spacewalks on crewed missions. The basic difference to Vostok was the elimination of the ejector seat to make room for two cosmonauts in spacesuits. To soften the landing, a solid fuel retro rocket was incorporated. Also a solid fuel back-up retro rocket system was carried in front of the spherical reentry capsule. The Voskhod launcher works normally and places its payload in an orbit 165km x 427km x 64 °. Immediately, the ground engineers receive video images enabling them to see that the Volga airlock deploys correctly and that the exterior hatch opens and closes as expected. But at the start of the third orbit, contact was suddenly lost by the three tracking stations that were in sight of Cosmos 57. The engineers quickly understood that the ship's self-destruct system had been activated. Following the explosion, 168 pieces were spotted on the radar. They will all enter the atmosphere between March 31 and April 6, 1965. The cause of the malfunction is quickly identified. Before launch, technicians noted that the exterior hatch might not close completely normally if there was no pressure difference between the exterior and the interior. It was therefore decided that once the ship was in orbit, the order to close the hatch (order #42) would be sent twice, not just once. However, a 3KD operating procedure gives a correspondence between a doubled order n°42 and a n°5 order (order n°5 orders atmospheric re-entry). Clearly, if the hatch is asked to close twice, the ship understands that it must enter the atmosphere. When the IP-7 station from Elizovo sends the famous order No. 42 to close the hatch, the IP-6 station from Klioutchi does the same. The spacecraft understands that it must turn on its braking motor to begin its return to Earth.

Low Earth Orbit

1 Payload

5,682 kilograms

Rocket

Retired
Voskhod

Active 1963 to 1976

OKB-1 logo

Manufacturer

OKB-1

Rocket

Height: 44.63m

Payload to Orbit

LEO: 6,001 kg

GTO: 0 kg

Liftoff Thrust

4,616 Kilonewtons

Fairing

Diameter: 2.58m

Height: 7.14m

Stages

3

Strap-ons

4

Launch Site

Site 1/5

Baikonur Cosmodrome, Kazakhstan

Fastest Turnaround

23 hr 32 min

Stats

Voskhod


7th

Mission

1st

Mission of 1965

OKB-1


117th

Mission

6th

Mission of 1965

1965


15th

Orbital launch attempt