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Centaur RL10 — NASA Sp8089 Injector Designs
98.5 %, 15,000 lbf, 400 psi
Centaur RL10 nasa sp8089 injector designs reference data. This dataset covers 1 row. Key parameters: num elements oxidizer 216 dimensionless; eta c 98.5 %; injector diameter in 10.3 in.
- Body Material
- 347 Cres
- Chamber Pressure Psi (psi)
- 400
- Combustion Stabilization
- None
- Element Type
- Coaxial
- Engine Designation
- RL10A-3
- Eta C Basis
- Shifting
- Eta C Pct (%)
- 98.5
- Face Material
- 347 Cres Rigimesh
- Injector Diameter in (in)
- 10.3
- Num Elements Oxidizer (dimensionless)
- 216
- Orifice Dia Fuel in (in)
- 0.017 Annulus
- Orifice Dia Oxidizer in (in)
- 0.079
- Propellants
- LOX/H2
- Thrust Condition
- Vac
- Thrust Lbf (lbf)
- 15,000
- Vehicle
- Centaur