Redmond Hydrazine rocket engine. 0.090 kN. Small ICBM. In Production. Developed as an attitude control thruster for the small ICBM. Isp=229s.

Application: Small ICBM.

Engine: 0.41 kg (0.90 lb). Chamber Pressure: 12.40 bar. Area Ratio: 15. Restarts: 1911.

Status: In Production.
Height: 0.15 m (0.49 ft).
Diameter: 0.0420 m (0.1370 ft).
Thrust: 90 N (20 lbf).
Specific impulse: 229 s.
Burn time: 150 s.

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