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-2100
Part of J-2
RS-2100
RS-2100
Credit: Boeing / Rocketdyne
Rocketdyne LOx/LH2 rocket engine. Next Generation Launch Vehicle Booster. Full flow staged combustion, pump-fed. Thrust and specific impulse values are at sea level.

Date: 1999. Thrust: 2,047.60 kN (460,319 lbf). Specific impulse: 384 s. Specific impulse sea level: 384 s.

Thrust (sl): 2,047.600 kN (460,319 lbf). Thrust (sl): 208,800 kgf.



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

Back to top of page
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
© 1997-2019 Mark Wade - Contact
© / Conditions for Use