RS-XXX
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 concept for Next Generation Delta with 7 m diameter modules.
Thrust (sl): 7,150.000 kN (1,607,380 lbf). Thrust (sl): 730,000 kgf.
Related
- Country
- USA
- Propellants
- Lox/LH2
- Agency
- Rocketdyne