Encyclopedia Astronautica

N2O4/MMH propellant rocket stage. Loaded mass 1,000 kg. Thrust 1.40 kN.

Status: Active.
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).

More... - Chronology...

Associated Engines
  • 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...

Associated Propellants
  • 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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