N2O4/UDMH propellant rocket stage. Loaded mass 2,000 kg.
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Gross mass: 2,000 kg (4,400 lb).
Height: 4.50 m (14.70 ft).
Diameter: 0.80 m (2.62 ft).
Number: 3 .
Associated Launch Vehicles
Jericho 1 Israeli short range ballistic missile. Follow-on version differed from original French-derived Jericho. Probably used a single 4500 kg solid-propellant motor. More...
Associated Manufacturers and Agencies
IAI Israeli manufacturer of rockets, spacecraft, and rocket engines. Israel Aircraft Industries, Israel. 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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