N2O4/UDMH propellant rocket stage. Loaded/empty mass 11,894/2,099 kg. Thrust 274.00 kN. Vacuum specific impulse 277 seconds.
Cost $ : 1.500 million. No Engines: 4.
More... - Chronology...
Status: Retired 1971.
Gross mass: 11,894 kg (26,221 lb).
Unfuelled mass: 2,099 kg (4,627 lb).
Height: 5.70 m (18.70 ft).
Diameter: 2.00 m (6.50 ft).
Span: 2.00 m (6.50 ft).
Thrust: 274.00 kN (61,597 lbf).
Specific impulse: 277 s.
Specific impulse sea level: 240 s.
Burn time: 96 s.
Number: 6 .
Vexin A SEP N2O4/UDMH rocket engine. 68.6 kN. Isp=277s. Used on Europa launch vehicle. First flight 1964. More...
Associated Launch Vehicles
ELDO A European orbital launch vehicle. Three stage version of the Europa vehicle. More...
Europa European orbital launch vehicle. Europe's first space launcher. The first stage was a British Blue Streak IRBM, the second stage the French Coralie, and the third stage the German Astris. All orbital launch attempts failed due to unreliability of the third stage. The project was cancelled after withdrawal of British support and replaced by the Ariane. More...
Cora European orbital launch vehicle. Cora was an experimental rocket to test the second and third stages of the Europa launch vehicle. More...
Europa II European orbital launch vehicle. Four stage version of the Europa vehicle, adding a P068 fourth stage. 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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