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MR-501B
Part of MR-500 engine series Family
MR-501B
MR-501B
Credit: Aerojet Redmond
Redmond Hydrazine rocket engine. BSAT-2 communications satellite. In Production. Electrothermal hydrazine thruster (EHT). 493 W input power at 24 V DC.

Status: In Production. Thrust: 0.37 N (0.08 lbf). Unfuelled mass: 0.89 kg (1.96 lb). Specific impulse: 303 s. Burn time: 14,000 s. Height: 0.20 m (0.65 ft). Diameter: 0.10 m (0.33 ft).

Engine: 0.89 kg (1.96 lb). Restarts: 500000.



Family: Storable liquid. Country: USA. Agency: Redmond.

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