HiPAT
Engine · USA
Original archive entry. The text, images and links below are kept as they were written.
Credit: Aerojet Redmond
Redmond N2O4/MMH rocket engine. In Production. High performance liquid apogee thruster.
Engine: 5.20 kg (11.40 lb). Chamber Pressure: 9.40 bar. Area Ratio: 375. Restarts: 500.
Related
- Family
- Storable liquid
- Country
- USA
- Propellants
- N2O4/MMH
- Agency
- Redmond
Photo Gallery
HiPAT Dual Thrust
Credit: Aerojet Redmond
