N2O4/MMH propellant rocket stage. Loaded mass 1,000 kg. Thrust 1.40 kN.
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Gross mass: 1,000 kg (2,200 lb).
Height: 1.00 m (3.20 ft).
Diameter: 1.32 m (4.33 ft).
Thrust: 1.40 kN (315 lbf).
RS-14 Rocketdyne N2O4/MMH rocket engine. 1.392 kN. Minuteman Postboost Velocity Control. Pressure-fed. Isp=315s. First flight 1970. More...
Associated Launch Vehicles
Minuteman 3 American four-stage solid-propellant intercontinental ballistic missile. In the 21st Century, the sole remaining US ICBM. More...
Associated Manufacturers and Agencies
Bell American manufacturer of rockets, spacecraft, and rocket engines. ARC Liquid Propellant Division, Niagara Falls, NY, USA. More...
N2O4/MMH Nitrogen tetroxide became the storable liquid propellant of choice from the late 1950's. Monomethylhydrazine (CH3NHNH2) is a storable liquid fuel that found favour in the United States for use in orbital spacecraft engines. Its advantages in comparison to UDMH are higher density and slightly higher performance. More...
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