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
L-7.70
Notional LOx/Kerosene rocket engine. Study 1963. Engines used in recoverable stage; separation at 3,365 m/s at 89,300 m altitude; splashdown using retrorockets under 8 46 m diameter parachutes 1300 km downrange.

Status: Study 1963. Thrust: 37,007.00 kN (8,319,504 lbf). Specific impulse: 335 s. Specific impulse sea level: 310 s. Burn time: 203 s.



Country: USA. Launch Vehicles: Nova GD-F. Propellants: Lox/Kerosene. Stages: Nova GD-F-1.

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