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Lance Sustainer — NASA Sp8089 Injector Designs
91.8 %, 4,000 lbf, 930 psi
Lance sustainer nasa sp8089 injector designs reference data. This dataset covers 1 row. Key parameters: num elements oxidizer 108 dimensionless; eta c 91.8 %; injector diameter in 5 in.
- Body Material
- Tens-50 Aluminum
- Chamber Pressure Psi (psi)
- 930
- Combustion Stabilization
- Acoustic Absorbers
- Element Type
- Unlike Doublet (pintle)
- Eta C Basis
- Shifting
- Eta C Pct (%)
- 91.8
- Face Material
- 347 Cres
- Injector Diameter in (in)
- 5
- Num Elements Oxidizer (dimensionless)
- 108
- Orifice Dia Oxidizer in (in)
- 0.060
- Propellants
- IRFNA/UDMH
- Thrust Lbf (lbf)
- 4,000
- Vehicle
- Lance (XRL) Sustainer