PRS-101
Engine · USA
Original archive entry. The text, images and links below are kept as they were written.
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.
Electrical Input Power: 0.10 kW. Engine: 4.74 kg (10.44 lb).
Related
- Country
- USA
- Propellants
- Electric/Teflon
- Agency
- Redmond