Nova GD-J-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 of ballistic shape; separation at 3,420 m/s at 93,900 m altitude; splashdown using retrorockets under 7 parachutes 1340 km downrange.
No Engines: 4.
Related
- Country
- USA
- Engines
- L-6.55
- Launch Vehicles
- Nova GD-J
- Propellants
- Lox/Kerosene