Saturn LCB-Alumizine-250 stage
Stage · USA
Original archive entry. The text, images and links below are kept as they were written.
N2O4/Alumizine propellant rocket stage. Boeing Low-Cost Saturn Derivative Study, 1967 (trade study of 260 inch first stages for S-IVB, all delivering 86,000 lb payload to LEO): Low Cost Booster, Single Pressure-fed N2O4/Alumizine Propellant engine, Ni-250 Hull.
Related
- Country
- USA
- Engines
- PF N204/Alumizine-1925k
- Launch Vehicles
- Saturn LCB-Alumizine-250
- Propellants
- N2O4/Alumizine