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| Volume 13, Number 1 2006 Facility Focus Highlighting a NASA Facility That Provides Function Beyond Space Exploration Propulsion Systems Laboratory (PSL)
Altitudes to 90,000 feet and Mach numbers to 3.0 in one cell and 6.0 in the other can be simulated continuously. Engine airflow is available to 480 lb/s at an inlet pressure of 55 psia or to 380 lb/s at 165 psia. Inlet temperature control also is available. Real-time display and post-test data reduction are available for all measured and calculated parameters. The PSL is a highly versatile test facility developed to suit the one-of-a-kind testing common to NASA aeronautics research and testing programs. This versatility allows quick reaction to changes in program direction, as well as complete flexibility to pursue new goals that arise unexpectedly from ongoing experimental research. Unique concepts in altitude engine testing have been pioneered and perfected in the PSL, such as multiaxis thrust measurement, vectored and reverse exhaust gas collection, infrared imaging at altitude, aeroelastic measurements, transient pressure and/or temperature distortion simulation and flight transient simulation. Recognizing innovation, other test organizations have asked to share PSL’s expertise.
The form also is available in electronic format for offline submission. For more information, visit http://facilities.grc.nasa.gov. Please mention that you read about it in Technology Innovation. |
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