Rocket Engine Components Testing
Test of the fuel regulator
- Pressure: 230 bar
- Flow: 638 lpm
- Operating fluid: jet fuel
- Control and regulation systems
- Pressure differential control
Valve Testing
- Pressure: 50 bar
- Flow: 21 000 lpm
- Power: 4 MW
- Gas generant performance test
- Operation fluid - water
Fuel Nozzle Test
- Operating fluid - jet fuel
- Spray cone 65…90°
- Deflection of spray cone with regard to an nozzle axis <2°
- Spray cone divergency detection
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