Redmond Hydrazine rocket engine. 254 mN. In Production. Low-voltage bus arcjet system. Input power 1780 W at 35 V DC. Isp=502s.

Engine: 7.23 kg (15.93 lb). Restarts: 1170.

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: 502 s.
Burn time: 3,780,000 s.

---