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Saturn Ib H1 — NASA Sp8089 Injector Designs
97.3 %, 204,300 lbf, 705 psi
Saturn IB H1 nasa sp8089 injector designs reference data. This dataset covers 1 row. Key parameters: num elements oxidizer 365 dimensionless; num elements fuel 612 dimensionless; eta c 97.3 %.
- Body Material
- 347 Cres
- Chamber Pressure Psi (psi)
- 705
- Combustion Stabilization
- Copper Baffles 7 Compartments
- Element Type
- Like Doublet and Triplet
- Engine Designation
- H-1
- Eta C Pct (%)
- 97.3
- Face Material
- Ofhc Copper
- Injector Diameter in (in)
- 20.9
- Num Elements Fuel (dimensionless)
- 612
- Num Elements Oxidizer (dimensionless)
- 365
- Orifice Dia Fuel in (in)
- 0.082
- Orifice Dia Oxidizer in (in)
- 0.120
- Propellants
- LOX/RP-1
- Thrust Condition
- Sl
- Thrust Lbf (lbf)
- 204,300
- Vehicle
- Saturn Ib