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-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.

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
© 1997-2017 Mark Wade - Contact
© / Conditions for Use