RS-800

Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9
A- B- C- D- E- F- G- H- I- J- K- L- M- N- O- P- Q- R- S- T- U- V- W- X- Y- Z

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.

Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9
A- B- C- D- E- F- G- H- I- J- K- L- M- N- O- P- Q- R- S- T- U- V- W- X- Y- Z