Nitric acid/UDMH propellant rocket stage. Loaded/empty mass 1,100,000/140,000 kg. Thrust 28,257.80 kN. Vacuum specific impulse 257 seconds.
No Engines: 29.
Status: Study 1952.
More... - Chronology...
Gross mass: 1,100,000 kg (2,400,000 lb).
Unfuelled mass: 140,000 kg (300,000 lb).
Height: 22.20 m (72.80 ft).
Diameter: 11.70 m (38.30 ft).
Span: 36.00 m (118.00 ft).
Thrust: 28,257.80 kN (6,352,606 lbf).
Specific impulse: 257 s.
Specific impulse sea level: 217 s.
Burn time: 84 s.
Associated Launch Vehicles
Von Braun 1956 German winged orbital launch vehicle. In 1956, for the book Exploration of Mars and the Disney television series, the 1952 design was significantly 'down-sized'. The first and second stages were simply reduced to 20% of their former size. A tiny expendable third stage replaced the manned glider. The manned glider itself became a seperate payload, that could be replaced by an 'all cargo' module. More...
Nitric acid/UDMH Drawing on the German World War II Wasserfall rocket, nitric acid (HNO3) became the early storable oxidiser of choice for missiles and upper stages of the 1950's. To overcome various problems with its use, it was necessary to combine the nitric acid with N2O4 and passivation compounds. These formulae were considered extremely secret at the time. By the late 1950's it was apparent that N2O4 by itself was a better oxidiser. Therefore nitric acid was almost entirely replaced by pure N2O4 in storable liquid fuel rocket engines developed after 1960. 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...
Home - Browse - Contact
© / Conditions for Use