Kosberg N2O4/UDMH rocket engine. 29 kN. P-700 Granit. Out of Production. Staged combustion cycle. Isp=275s. First flight 1970.
Application: P-700 Granit.
Engine: 28 kg (61 lb). Chamber Pressure: 123.00 bar. Thrust to Weight Ratio: 105.71.
Status: Out of Production.
More... - Chronology...
Unfuelled mass: 28 kg (61 lb).
Height: 0.60 m (1.96 ft).
Diameter: 0.15 m (0.49 ft).
Thrust: 29.00 kN (6,519 lbf).
Specific impulse: 275 s.
Burn time: 16 s.
First Launch: 1968-70.
Granat Russian x-ray astronomy satellite. One launch, 1989.12.01. Granat was a Lavochkin design with the mission of making gamma ray observations in energy ranges of 3 to 200 keV. More...
Associated Manufacturers and Agencies
Kosberg Russian manufacturer of rocket engines. Kosberg Design Bureau, Russia. 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...
Haeseler, Dietrich, Visit to the museum of Chemical Automatics Design Bureau, Voronezh 1992 via Dietrich Haeseler.
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