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
PW 1000000 lb LH2
Part of Cobra
Pratt and Whitney LOx/LH2 rocket engine. Study 1988. Part of launch vehicle proposed by Martin as alternative to NLS. All figures estimated based on 1,000,000 lb thrust single engine.

Status: Study 1988. Thrust: 4,457.00 kN (1,001,973 lbf). Specific impulse: 425 s. Specific impulse sea level: 354 s. Burn time: 420 s.



Country: USA. Launch Vehicles: Titan 5. Propellants: Lox/LH2. Stages: Titan 5 stage. Agency: Pratt and Whitney.

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