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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.
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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
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