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Saturn Ic F1 — NASA Sp8089 Injector Designs
93.8 %, 1,522,000 lbf, 1,128 psi
Saturn IC F1 nasa sp8089 injector designs reference data. This dataset covers 1 row. Key parameters: num elements oxidizer 714 dimensionless; num elements fuel 702 dimensionless; eta c 93.8 %.
- Body Material
- 347 Cres
- Chamber Pressure Psi (psi)
- 1,128
- Combustion Stabilization
- Copper Baffles 13 Compartments
- Element Type
- Like Doublet
- Engine Designation
- F-1
- Eta C Pct (%)
- 93.8
- Face Material
- Ofhc Copper
- Injector Diameter in (in)
- 39.2
- Num Elements Fuel (dimensionless)
- 702
- Num Elements Oxidizer (dimensionless)
- 714
- Orifice Dia Fuel in (in)
- 0.281
- Orifice Dia Oxidizer in (in)
- 0.242
- Propellants
- LOX/RP-1
- Thrust Condition
- Sl
- Thrust Lbf (lbf)
- 1,522,000
- Vehicle
- Saturn Ic