Russian manned spacecraft module. Cancelled 1965. Calculated masses, specific impulse based on mission requirements and drawing of spacecraft. Equipment-engine section.
AKA: Priborno-agregatniy otsek.
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Gross mass: 16,000 kg (35,000 lb).
Unfuelled mass: 3,000 kg (6,600 lb).
Height: 4.70 m (15.40 ft).
Diameter: 2.90 m (9.50 ft).
Specific impulse: 310 s.
LK-1 Russian manned lunar flyby spacecraft. Cancelled 1965. The LK-1 was the spacecraft designed by Chelomei for the original Soviet manned lunar flyby project. More...
N2O4/UDMH Nitrogen tetroxide became the storable liquid propellant of choice from the late 1950's. Unsymmetrical Dimethylhydrazine ((CH3)2NNH2) became the storable liquid fuel of choice by the mid-1950's. Development of UDMH in the Soviet Union began in 1949. It is used in virtually all storable liquid rocket engines except for some orbital manoeuvring engines in the United States, where MMH has been preferred due to a slightly higher density and performance. More...
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