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Titan I Booster — NASA Sp8089 Injector Designs
97.8 %, 180,000 lbf, 637 psi
Titan I booster nasa sp8089 injector designs reference data. This dataset covers 1 row. Key parameters: num elements oxidizer 560 dimensionless; num elements fuel 610 dimensionless; eta c 97.8 %.
- Body Material
- 347 Cres
- Chamber Pressure Psi (psi)
- 637
- Combustion Stabilization
- None
- Element Type
- Like Doublet
- Eta C Pct (%)
- 97.8
- Face Material
- 347 Cres
- Injector Diameter in (in)
- 21.6
- Num Elements Fuel (dimensionless)
- 610
- Num Elements Oxidizer (dimensionless)
- 560
- Orifice Dia Oxidizer in (in)
- 0.119
- Propellants
- LOX/RP-1
- Thrust Condition
- Sl
- Thrust Lbf (lbf)
- 180,000
- Vehicle
- Titan I Booster