RS-800
Engine · USA
Original archive entry. The text, images and links below are kept as they were written.
Rocketdyne LOx/LH2 rocket engine. Design concept -2004. New high-thrust cryogenic engine for Delta IV Heavy growth versions.
Thrust (sl): 3,569.000 kN (802,343 lbf). Thrust (sl): 364,000 kgf.
Related
- Country
- USA
- Propellants
- Lox/LH2
- Agency
- Rocketdyne