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The
Propulsion Systems Laboratory is NASA's only ground-based test facility
that can provide true flight simulation for experimental research
on air-breathing propulsion systems.
Characteristics
and Performance
- Altitude simulation to 90,000 ft
- Two
engine test cells: PSL-3 and PSL-4
- Mach
Number Range:
- PSL-3:
to 3.0
- PSL-4:
to 4.0
- PSL-4:
Freejet Mach No. with auxiliary heater - to 6.0
- Tied
to central compressed air and exhaust systems
- Thrust
measurement: 50,000 lbf horizontal axis, 15,000 lbf vertical and
lateral axes
Combustion
Air System
- Main
Supply
- 480
lbs/sec @ ambient temperature and 55 psia
- 380
lbs/sec @ ambient temperature and 165 psia
- 240
lbs/sec @ 1100°F and 165 psia
- 380
lbs/sec @ -40°F and 25 psia (PSL-3)
- 30
lbs/sec @ -90°F and 25 psia (PSL-4)
- Cooling
Air Supply
- 100
lbs/sec @ ambient temperature and 55 psia to 165 psia
Altitude
Exhaust System
- Altitude
Range: sea level standard to 90,000 ft
- Mass
Flow: up to 750 lbs/sec
Support
Systems
- Jet
Fuel System: Two 25,000 gallon tanks supporting various types
of fuel (JET-A, JP-4, JP-5, JP-8)
- Natural
Gas system: 10 inch header @ 50 psig
- Gaseous
Hydrogen System: 1 lb/sec @ 600 psig -- 3 lbs/sec @ 1100 psig,
maximum pressure is 2400 psig
- Gaseous
Oxygen System: 3 lbs/sec @ 1200 psig, 10 lbs/sec @ 400 psig, maximum
pressure is 2400 psig
- Gaseous
Nitrogen System: 132,000 scf @ 2400 psig
- Hydraulic
System: 100 gpm @ 3000 psig
- High
Pressure Hydraulic System: 100 gpm @ 6000 psig
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NASA's ATP Program
Read about one of the largest, most versatile and comprehensive set of testing facilities in the nation.
+ View the fact sheet (PDF) |
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Propulsion Systems Laboratory (PSL)
Provides true flight simulation for air-breathing propulsion
+ View the fact sheet (PDF) |
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GRC Research Facilities
Find out more about the research facilities at NASA's Glenn Research Center
+ View the site |
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"The right facility at the right time" - NASA Aeronautics Test Program |
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