Nitric acid/UDMH rocket stage. 570.00 kN (128,141 lbf) thrust. Mass 25,600 kg (56,438 lb).
More... - Chronology...
Gross mass: 25,600 kg (56,400 lb).
Unfuelled mass: 3,700 kg (8,100 lb).
Height: 12.00 m (39.00 ft).
Diameter: 1.30 m (4.20 ft).
Thrust: 570.00 kN (128,140 lbf).
Burn time: 95 s.
Number: 1 .
Nodong North Korean Nitric acid/UDMH rocket engine. 144 kN. In production. Isp=255s. Used in North Korean missiles and Taepodong 1 satellite launcher. Derived from Isayev designs developed for Scud missiles and SLBM's of the Makeyev bureau. First flight 1998. More...
Associated Launch Vehicles
Taepodong 2 North Korean intermediate range ballistic missile. Two-stage ballistic missile. First stage is 18 m long, second is 14 m long. More...
Associated Manufacturers and Agencies
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