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MR-510
Part of MR-500 engine series
MR-510
MR-510
Credit: Aerojet Redmond
Redmond Hydrazine rocket engine. In Production. Arcjet system.

Status: In Production. Thrust: 0.25 N (0.06 lbf). Unfuelled mass: 1.58 kg (3.48 lb). Specific impulse: 600 s. Burn time: 6,228,000 s. Height: 0.25 m (0.82 ft). Diameter: 0.0430 m (0.1410 ft).

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



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

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