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Apollo Lem Descent — NASA Sp8089 Injector Designs
96.2 %, 9,850 lbf, 104 psi
Apollo LEM descent nasa sp8089 injector designs reference data. This dataset covers 1 row. Key parameters: num elements oxidizer 36 dimensionless; num elements fuel 1 dimensionless; eta c 96.2 %.
- Body Material
- Titanium
- Chamber Pressure Psi (psi)
- 104
- Combustion Stabilization
- None
- Element Type
- Coaxial Pintle
- Eta C Basis
- Shifting
- Eta C Pct (%)
- 96.2
- Face Material
- Titanium and Columbium
- Injector Diameter in (in)
- 13.2
- Num Elements Fuel (dimensionless)
- 1
- Num Elements Oxidizer (dimensionless)
- 36
- Orifice Dia Fuel in (in)
- Variable
- Orifice Dia Oxidizer in (in)
- Variable
- Propellants
- N2O4/A-50
- Thrust Condition
- Vac
- Thrust Lbf (lbf)
- 9,850
- Vehicle
- Apollo Lunar Descent