| MR-501 |
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Engine Model: MR-501B. Designer: Aerojet Redmond. Application: BSAT-2 communications satellite. Propellants: Hydrazine. Thrust(vac): 0.37 N (0.08 lbf). Isp: 303 sec. Burn time: 14,000 sec. Mass Engine: 0.89 kg (1.96 lb). Diameter: 0.10 m (0.33 ft). Length: 0.20 m (0.65 ft). Chambers: 1. Country: USA. Status: In Production. Electrothermal hydrazine thruster (EHT). 493 W input power at 24 V DC. Contact us with any corrections, additions, or comments. Conditions for use of drawings, pictures, or other materials from this site.. To contact astronauts or cosmonauts. © Mark Wade, 1997 - 2008 except where otherwise noted. |
