Nova GD-F-1
Stage · USA
Original archive entry. The text, images and links below are kept as they were written.
LOx/Kerosene propellant rocket stage. Massed estimated based on tank volumes, total thrust, and first stage burnout conditions. 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.
No Engines: 4.
Related
- Country
- USA
- Engines
- L-7.70
- Launch Vehicles
- Nova GD-F
- Propellants
- Lox/Kerosene