Volga (rocket stage)
Volga, GRAU index 14S46, also designated 141KS, is a rocket upper stage designed in Russia. It is used with the Soyuz-2.1a and Soyuz-2-1v rockets to insert payloads into sun-synchronous orbit. It is derived from the propulsion module of the Yantar spy satellites.[4] It is closely related to the retired Ikar upper stage.[3]
Manufacturer | TsSKB-Progress |
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Country of origin | Russia |
General characteristics | |
Diameter | 3.2 metres (10 ft) |
Length | 1.025 metres (3 ft 4.4 in) |
Propellant mass | 300–900 kilograms (660–1,980 lb) |
Empty mass | 840 kilograms (1,850 lb) |
Volga | |
Powered by | 1 17D64[2][3] (KB Melnikov) |
Maximum thrust | 2.94 kilonewtons (660 lbf) |
Specific impulse | 307 seconds (3.01 km/s) |
Burn time | 600 s |
Propellant | N2O4/UDMH |