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Apollo Sps — NASA Sp8089 Injector Designs
97.5 %, 21,500 lbf, 100 psi
Apollo SPS nasa sp8089 injector designs reference data. This dataset covers 1 row. Key parameters: num elements oxidizer 575 dimensionless; eta c 97.5 %; injector diameter in 17.6 in.
- Body Material
- 5083 Aluminum
- Chamber Pressure Psi (psi)
- 100
- Combustion Stabilization
- 5 Baffles + Hub
- Element Type
- Unlike Doublet
- Eta C Pct (%)
- 97.5
- Face Material
- 5083 Aluminum
- Injector Diameter in (in)
- 17.6
- Num Elements Oxidizer (dimensionless)
- 575
- Orifice Dia Fuel in (in)
- 0.041-0.077
- Orifice Dia Oxidizer in (in)
- 0.041-0.073
- Propellants
- N2O4/A-50
- Thrust Condition
- Vac
- Thrust Lbf (lbf)
- 21,500
- Vehicle
- Apollo Sps