Redmond Hydrazine rocket engine. 254 mN. In Production. Arcjet system. Isp=600s.

Engine: 1.58 kg (3.48 lb). Restarts: 1950.

Status: In Production.
Height: 0.25 m (0.82 ft).
Diameter: 0.0430 m (0.1410 ft).
Thrust: 0.25 N (0.06 lbf).
Specific impulse: 600 s.
Burn time: 6,228,000 s.

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