P8E-9
Engine · USA
Original archive entry. The text, images and links below are kept as they were written.
Credit: Boeing / Rocketdyne
Rocketdyne Nitric acid/UDMH rocket engine. Lance Booster and Sustainer System. Pressure-fed. Sustainer 4400 -14,400 lbf, 227 sec Isp. Thrust and specific impulse values are at sea level. First flight 1972.
Thrust (sl): 205.440 kN (46,185 lbf). Thrust (sl): 20,950 kgf. Propellant Formulation: IRFNA/UDMH.
Related
- Family
- Storable liquid
- Country
- USA
- Propellants
- Nitric acid/UDMH
- Agency
- Rocketdyne