Encyclopedia Astronautica
MRM-106



mrm106b.jpg
MRM-106B
Credit: Aerojet Redmond
mrm106c.jpg
MRM-106C
Credit: Aerojet Redmond
mrm106d.jpg
MRM-106D
Credit: Aerojet Redmond
mrm106e.jpg
MRM-106E
Credit: Aerojet Redmond
mrm106f.jpg
MRM-106F
Credit: Aerojet Redmond
Redmond Hydrazine rocket engine. 0.027 kN. In Production. Steady-state thrust 9 N. Isp=231s.

Engine: 0.94 kg (2.07 lb). Restarts: 1570.

Status: In Production.
Unfuelled mass: 0.94 kg (2.07 lb).
Height: 0.17 m (0.56 ft).
Diameter: 0.0310 m (0.1010 ft).
Thrust: 27 N (6 lbf).
Specific impulse: 231 s.
Burn time: 2,991 s.

More... - Chronology...


Associated Countries
See also
Associated Manufacturers and Agencies
  • Redmond American manufacturer of rocket engines. Redmond, USA. More...

Associated Propellants
  • Hydrazine Hydrazine (N2H4) found early use as a fuel, but it was quickly replaced by UDMH. It is still used as a monopropellant for satellite station-keeping motors. Hydrazine (N2H4) found early use as a fuel, but it was quickly replaced by UDMH. It is still used as a monopropellant for satellite station-keeping motors. More...

Home - Browse - Contact
© / Conditions for Use