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Advanced Subsonic Combustion Rig (ASCR)
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Quick Facts
Capabilities
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Facility Fact

The ASCR supports research on multiple fuel injector test hardware for large aircraft engine development, and full-scale annular combustor development for regional aircraft engines.

C-1999-251: Technicians in front of the ASCR C-1999-249: Technicians setting up a test in the ASCR
Facility Capabilities
Features
  • Inlet pressure: 150 to 900 psig
  • Inlet temperature: 250 to 1300 °F
  • Inlet airflow : 5 to 50 lb/s
  • Exhaust: atmospheric

Stand 1 Sector Rig Capabilities

  • Fuel Lines: 10
  • Gas Analysis: 20 sample lines
  • Pressure Measurements: 60 P taps
  • Temperature Measurements: 96 Type K/12 Type B
  • Ignition Source: spark igniter

Stand 2 Flametube Capabilities

  • Fuel Lines: 4
  • Gas Analysis: 2 sample lines
  • Pressure Measurements: 60 P taps
  • Temperature Measurements: 96 Type K/12 Type B
  • Ignition Source: spark igniter

Other Features

  • Dynamic Pressure Measurement
  • Laser diagnostic capabilties
Further Information
Advanced Subsonic Combustion Rig (ASCR)
A high-pressure, high temperature combustion rig
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Last Updated: January 24, 2007