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Titan II STAGE2 — NASA Sp8089 Injector Designs
97.4 %, 100,000 lbf, 827 psi
Titan II stage2 nasa sp8089 injector designs reference data. This dataset covers 1 row. Key parameters: num elements oxidizer 1,319 dimensionless; num elements fuel 818 dimensionless; eta c 97.4 %.
- Body Material
- 347 Cres
- Chamber Pressure Psi (psi)
- 827
- Combustion Stabilization
- 6 Baffles + Hub
- Element Type
- Quadlet
- Eta C Pct (%)
- 97.4
- Face Material
- 347 Cres
- Injector Diameter in (in)
- 14.5
- Num Elements Fuel (dimensionless)
- 818
- Num Elements Oxidizer (dimensionless)
- 1,319
- Orifice Dia Fuel in (in)
- 0.037
- Orifice Dia Oxidizer in (in)
- 0.049
- Propellants
- N2O4/A-50
- Thrust Condition
- Vac
- Thrust Lbf (lbf)
- 100,000
- Vehicle
- Titan II Stage 2