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Atlas MA5 Booster — NASA Sp8089 Injector Designs
95.5 %, 165,000 lbf, 577 psi
Atlas MA5 booster nasa sp8089 injector designs reference data. This dataset covers 1 row. Key parameters: num elements oxidizer 335 dimensionless; num elements fuel 582 dimensionless; eta c 95.5 %.
- Body Material
- 347 Cres
- Chamber Pressure Psi (psi)
- 577
- Combustion Stabilization
- Copper Baffles 7 Compartments
- Element Type
- Like Doublet and Triplet
- Eta C Pct (%)
- 95.5
- Face Material
- Ofhc Copper
- Injector Diameter in (in)
- 20.9
- Num Elements Fuel (dimensionless)
- 582
- Num Elements Oxidizer (dimensionless)
- 335
- Orifice Dia Fuel in (in)
- 0.0635
- Orifice Dia Oxidizer in (in)
- 0.113
- Propellants
- LOX/RP-1
- Thrust Condition
- Sl
- Thrust Lbf (lbf)
- 165,000
- Vehicle
- Atlas Ma-5 Booster