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Atlas MA5 Sustainer — NASA Sp8089 Injector Designs
96.4 %, 57,000 lbf, 706 psi
Atlas MA5 sustainer nasa sp8089 injector designs reference data. This dataset covers 1 row. Key parameters: num elements oxidizer 144 dimensionless; num elements fuel 175 dimensionless; eta c 96.4 %.
- Body Material
- 4130 Steel
- Chamber Pressure Psi (psi)
- 706
- Combustion Stabilization
- None
- Element Type
- Like Triplet
- Eta C Pct (%)
- 96.4
- Face Material
- 4130 Steel
- Injector Diameter in (in)
- 12.4
- Num Elements Fuel (dimensionless)
- 175
- Num Elements Oxidizer (dimensionless)
- 144
- Orifice Dia Fuel in (in)
- 0.0935
- Orifice Dia Oxidizer in (in)
- 0.120
- Propellants
- LOX/RP-1
- Thrust Condition
- Sl
- Thrust Lbf (lbf)
- 57,000
- Vehicle
- Atlas Ma-5 Sustainer