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Titan II Booster — NASA Sp8089 Injector Designs
97.2 %, 215,000 lbf, 785 psi
Titan II booster nasa sp8089 injector designs reference data. This dataset covers 1 row. Key parameters: num elements oxidizer 568 dimensionless; num elements fuel 516 dimensionless; eta c 97.2 %.
- Body Material
- 347 Cres
- Chamber Pressure Psi (psi)
- 785
- Combustion Stabilization
- None
- Element Type
- Like Doublet
- Eta C Pct (%)
- 97.2
- Face Material
- 347 Cres
- Injector Diameter in (in)
- 21.8
- Num Elements Fuel (dimensionless)
- 516
- Num Elements Oxidizer (dimensionless)
- 568
- Orifice Dia Fuel in (in)
- 0.082
- Orifice Dia Oxidizer in (in)
- 0.119
- Propellants
- N2O4/A-50
- Thrust Condition
- Sl
- Thrust Lbf (lbf)
- 215,000
- Vehicle
- Titan II Booster