RS-800 (original) (raw)

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RS-800

Part of RS-68

Rocketdyne LOx/LH2 rocket engine. Design concept -2004. New high-thrust cryogenic engine for Delta IV Heavy growth versions.

Status: Design concept -2004. Date: 2005. Thrust: 4,110.00 kN (923,960 lbf).

Thrust (sl): 3,569.000 kN (802,343 lbf). Thrust (sl): 364,000 kgf.

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

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