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PRS-101
PRS-101
PRS-101
Credit: Aerojet Redmond
Redmond electric/Teflon rocket engine. 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.

AKA: PRS. Status: In Production. Thrust: 0.0124 N (0.0027 lbf). Unfuelled mass: 4.74 kg (10.44 lb). Specific impulse: 1,350 s. Burn time: 2,500,000 s. Height: 0.29 m (0.94 ft). Diameter: 0.23 m (0.77 ft).

Electrical Input Power: 0.10 kW. Engine: 4.74 kg (10.44 lb).



Country: USA. Propellants: Electric/Teflon. Agency: Redmond.

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