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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