Russian manned spacecraft module. Study 1965. Auxilliary Retrorocket.
Spacecraft delta v: 60 m/s (196 ft/sec).
AKA: Engine unit.
Gross mass: 143 kg (315 lb).
Unfuelled mass: 56 kg (123 lb).
Height: 0.60 m (1.96 ft).
Diameter: 0.25 m (0.82 ft).
Thrust: 117.00 kN (26,302 lbf).
Specific impulse: 224 s.
More... - Chronology...
Associated Countries
Associated Spacecraft
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Voskhod Russian manned spacecraft. 5 launches, 1964.10.06 (Cosmos 47) to 1966.02.22 (Cosmos 110). More...
See also
Associated Propellants
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Solid Solid propellants have the fuel and oxidiser embedded in a rubbery matrix. They were developed to a high degree of perfection in the United States in the 1950's and 1960's. In Russia, development was slower, due to a lack of technical leadership in the area and rail handling problems. Solid propellants have the fuel and oxidiser embedded in a rubbery matrix. They were developed to a high degree of perfection in the United States in the 1950's and 1960's. In Russia, development was slower, due to a lack of technical leadership in the area and rail handling problems. More...
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