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RS-XXX
Rocketdyne LOx/LH2 rocket engine. Design concept -2004. New high-thrust cryogenic engine concept for Next Generation Delta with 7 m diameter modules.

Status: Design concept -2004. Date: 2005. Thrust: 8,230.00 kN (1,850,170 lbf).

Thrust (sl): 7,150.000 kN (1,607,380 lbf). Thrust (sl): 730,000 kgf.

Country: USA. Propellants: Lox/LH2. Agency: Rocketdyne.
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