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Lance Booster — NASA Sp8089 Injector Designs
93.4 %, 42,000 lbf, 950 psi
Lance booster nasa sp8089 injector designs reference data. This dataset covers 1 row. Key parameters: num elements fuel 460 dimensionless; eta c 93.4 %; thrust lbf 42,000 lbf.
- Body Material
- Tens-50 Aluminum
- Chamber Pressure Psi (psi)
- 950
- Combustion Stabilization
- Ablative Baffles and Acoustic Absorbers
- Element Type
- Unlike Doublet
- Eta C Basis
- Shifting
- Eta C Pct (%)
- 93.4
- Face Material
- Tens-50 Aluminum
- Num Elements Fuel (dimensionless)
- 460
- Orifice Dia Fuel in (in)
- 0.0515
- Orifice Dia Oxidizer in (in)
- 0.073
- Propellants
- IRFNA/UDMH
- Thrust Condition
- Sl
- Thrust Lbf (lbf)
- 42,000
- Vehicle
- Lance (XRL) Booster