| PRS-101 |
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Engine Model: PRS-101. Designer: Aerojet Redmond. Propellants: Electric/Teflon. Thrust(vac): 0.0012 N (0.0003 lbf). Isp: 1,350 sec. Burn time: 2,500,000 sec. Mass Engine: 4.74 kg (10.44 lb). Diameter: 0.23 m (0.77 ft). Length: 0.29 m (0.94 ft). Chambers: 1. Country: USA. Status: In Production. Pulsed plasma thruster system. Completely solid state propulsion. Up to 100 W input power at 28 V DC, thrust to power ratio 12.4 microN/W. 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. |
