Nova GD-B-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 engine package; separation at 3,398 m/s at 76,200 m altitude; splashdown using retrorockets under 7 30 m diameter parachutes 1300 km downrange.
No Engines: 16.
Related
- Country
- USA
- Engines
- F-1A
- Launch Vehicles
- Nova GD-B
- Propellants
- Lox/Kerosene