S-I stage
Stage · USA
Original archive entry. The text, images and links below are kept as they were written.
LOx/Kerosene propellant rocket stage. Configuration as flown, Saturn I.
Cost $ : 43.500 million. No Engines: 8.
Subtopics
Super-Jupiter stage LOx/Kerosene propellant rocket stage. Earliest member of what would become the Saturn family. Masses estimated.- Jupiter Cluster LOx/Kerosene propellant rocket stage. Masses estimated (cluster of four Jupiter IRBM stages).
- Saturn S-IB-2 LOx/Kerosene propellant rocket stage. .
- Saturn S-IB-4 LOx/Kerosene propellant rocket stage. .
- Saturn IB stage LOx/Kerosene propellant rocket stage. Configuration as flown, Saturn IB.
- Saturn S-IB-A LOx/Kerosene propellant rocket stage. Douglas Studies, 1965: S-1B with 225 k lbf H-1's.
- Saturn IB-11 LOx/Kerosene propellant rocket stage. 20 foot stretch of Saturn IB for use with UA1207 7 segment solid rocket strap-on units.
- Saturn IB-15 LOx/Kerosene propellant rocket stage. 10 foot stretch of Saturn IB. Not found useful in any configuration except with Minuteman first-stage strap-ons to augment thrust.
- Saturn S-1B-4 LOx/Kerosene propellant rocket stage. Chrysler Studies, 1966: S-1B with 4 H-1's for use with Titan UA1205 strap-ons.
Related
- Country
- USA
- Engines
- H-1 engine
- Launch Vehicles
- Juno V-A, Juno V-B, Saturn A-1, Saturn C-2, Saturn C-1, Saturn I Blk2, Saturn I
- Propellants
- Lox/Kerosene