Sea Dragon-1
Stage · USA
Original archive entry. The text, images and links below are kept as they were written.
LOx/Kerosene propellant rocket stage. Truax pressure fed design. Sea level thrust shown. Thrust, chamber pressure varies during ascent. Vacuum thrust at cut-off 40 million kgf. Total mass, specific impulse estimated from booster performance figures.
Related
- Country
- USA
- Engines
- Sea Dragon-1 engine
- Propellants
- Lox/Kerosene