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Ssme — NASA Sp8089 Injector Designs
99.6 %, 509,000 lbf, 3,250 psi
SSME nasa sp8089 injector designs reference data. This dataset covers 1 row. Key parameters: num elements oxidizer 600 dimensionless; eta c 99.6 %; injector diameter in 17.8 in.
- Body Material
- Inconel 718
- Chamber Pressure Psi (psi)
- 3,250
- Combustion Stabilization
- Baffles
- Element Type
- Coaxial
- Eta C Basis
- Shifting
- Eta C Pct (%)
- 99.6
- Face Material
- 347 Cres Rigimesh
- Injector Diameter in (in)
- 17.8
- Num Elements Oxidizer (dimensionless)
- 600
- Orifice Dia Fuel in (in)
- 0.065 Annulus
- Orifice Dia Oxidizer in (in)
- 0.188
- Propellants
- LOX/H2
- Thrust Condition
- Vac
- Thrust Lbf (lbf)
- 509,000
- Vehicle
- Ssme