Soyuz/Vostok

Last updated
  1. 1 2 Wade, Mark. "Soyuz". Encyclopedia Astronautica. Archived from the original on 2010-01-07. Retrieved 2009-04-15.
Soyuz/Vostok
FunctionInterim carrier rocket
Manufacturer OKB-1
Country of origin Soviet Union
Size
StagesThree
Capacity
Payload to LEO
Mass4,500 kilograms (9,900 lb)
Associated rockets
Family R-7
Launch history
StatusRetired
Launch sites Baikonur 31/6
Total launches2
Success(es)2
First flight27 December 1965
Last flight20 July 1966
People or cargo transported US-A
Boosters – Block A/B/V/G
No. boosters4
Powered by1 RD-107
Maximum thrust994.3 kilonewtons (223,500 lbf)
Specific impulse 315 sec
Burn time118 seconds
Propellant RP-1/LOX