Saturn IVB (S-IB)
Stage · USA
Original archive entry. The text, images and links below are kept as they were written.
LOx/LH2 propellant rocket stage. Saturn IB version of S-IVB stage. Due to lower payload, 300 kg saving in structure compared to Saturn V version. Due to deletion of restart requirement, 700 kg saving in propulsion system (primarily reduction in helium for restart).
Related
- Country
- USA
- Engines
- J-2
- Launch Vehicles
- Saturn IB, Saturn INT-05, Saturn INT-27, Saturn INT-05A, Saturn IB-C, Saturn IB-CE, Saturn IB-D, Uprated Saturn I, Saturn INT-11, Saturn INT-12, Saturn INT-13, Saturn INT-14, Saturn INT-15, Saturn INT-16, Saturn INT-17, Saturn INT-18, Saturn INT-19, Saturn V, Saturn LCB-Alumizine-140, Saturn LCB-Alumizine-250, Saturn LCB-Storable-140, Saturn LCB-Storable-250, Saturn LCB-Lox/RP-1, Saturn S-IC-TLB, Saturn LCB-SR
- Propellants
- Lox/LH2