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Saturn J2 — NASA Sp8089 Injector Designs
98.6 %, 230,000 lbf, 780 psi
Saturn J2 nasa sp8089 injector designs reference data. This dataset covers 1 row. Key parameters: num elements oxidizer 614 dimensionless; eta c 98.6 %; injector diameter in 18.5 in.
- Body Material
- Inconel 718
- Chamber Pressure Psi (psi)
- 780
- Combustion Stabilization
- Tuned Elements
- Element Type
- Coaxial
- Engine Designation
- J-2
- Eta C Pct (%)
- 98.6
- Face Material
- 347 Cres Rigimesh
- Injector Diameter in (in)
- 18.5
- Num Elements Oxidizer (dimensionless)
- 614
- Orifice Dia Fuel in (in)
- 0.049 Annulus
- Orifice Dia Oxidizer in (in)
- 0.182
- Propellants
- LOX/H2
- Thrust Condition
- Vac
- Thrust Lbf (lbf)
- 230,000
- Vehicle
- Saturn II and Ivb