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Agena LR81 — NASA Sp8089 Injector Designs
95.7 %, 15,800 lbf, 506 psi
Agena LR81 nasa sp8089 injector designs reference data. This dataset covers 1 row. Key parameters: eta c 95.7 %; injector diameter in 10.8 in; orifice dia oxidizer in 0.111 in.
- Body Material
- 6061 Aluminum
- Chamber Pressure Psi (psi)
- 506
- Combustion Stabilization
- None
- Element Type
- Triplet
- Engine Designation
- LR81-Ba-11
- Eta C Basis
- Shifting
- Eta C Pct (%)
- 95.7
- Face Material
- 6061 Aluminum
- Injector Diameter in (in)
- 10.8
- Num Elements Fuel (dimensionless)
- 176
- Num Elements Oxidizer (dimensionless)
- 88
- Orifice Dia Fuel in (in)
- 0.049
- Orifice Dia Oxidizer in (in)
- 0.111
- Propellants
- IRFNA/UDMH
- Thrust Condition
- Vac
- Thrust Lbf (lbf)
- 15,800
- Vehicle
- Agena