L-7.70
Engine · USA
Original archive entry. The text, images and links below are kept as they were written.
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.
Related
- Country
- USA
- Launch Vehicles
- Nova GD-F
- Propellants
- Lox/Kerosene
- Stages
- Nova GD-F-1