Saturn LCB-Lox/RP-1 stage
Stage · USA
Original archive entry. The text, images and links below are kept as they were written.
LOx/Kerosene 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 LOx/RFP-1 engine.
Related
- Country
- USA
- Engines
- PF RP-1
- Launch Vehicles
- Saturn LCB-Lox/RP-1
- Propellants
- Lox/Kerosene