L-5.25H
Engine · USA
Original archive entry. The text, images and links below are kept as they were written.
Notional LOx/LH2 rocket engine. Study 1963. Engines for recoverable booster engine package 'half stage' of a 1 1/2 stage arrangement. Used on Nova GD-H launch vehicle.
Separation at 2,980 m/s at 87,800 m altitude; splashdown under 4 46 m diameter parachutes 1,000 km downrange.
Related
- Country
- USA
- Launch Vehicles
- Nova GD-H
- Propellants
- Lox/LH2
- Stages
- Nova GD-H-0