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1'x1' Supersonic Wind Tunnel (1x1)
The 1x1 specializes in conducting fundamental research in supersonic and hypersonic research and detailed benchmark quality experiments.
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2.2 Second Drop Tower
The tower is used to study the effects of microgravity on combustion and fluid dynamics, and to develop technologies for space missions.
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8'x6' Supersonic Wind Tunnel (8x6)
The 8x6 is a world-class facility that provides researchers with the opportunity to explore higher speed regions of flight.
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9'x15' Low Speed Wind Tunnel (9x15)
This facility has unique and nationally recognized capabilities to evaluate many aerodynamic performance and acoustic characteristics.
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10'x10' Supersonic Wind Tunnel
This facility has unique and nationally recognized capabilities to evaluate many aerodynamic performance and acoustic characteristics.
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Aero-Acoustic Propulsion Laboratory (AAPL)
The AAPL is an acoustically treated geodesic dome that provides researchers an environment for acoustic testing of aeropropulsion components.
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Advanced Subsonic Combustion Rig (ASCR)
The ASCR contains two operational test stands that support low-emissions combustor research and development.
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Cryogenic Components Laboratory (CCL)
The CCL is a new, state-of-the-art facility for research, development and qualification of cryogenic materials, components and systems.
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Cryogenic Propellant Tank Facility (K-Site)
K-Site plays an essential role in the development of advanced insulation systems and on-orbit fluid transfer techniques for cryogenic fuel tanks.
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Electric Propulsion Laboratory (EPL)
The EPL provides large space environment chambers for the research and development of spacecraft power systems.
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Engine Components Research Laboratory
The ECRL has the capabilities and track record to perform high-quality, high-performance testing on combustor and afterburner concepts.
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Engine Propulsion Research Building (EPRB)
The EPRB supports research and development of spacecraft power, electric propulsion, and space environmental effects.
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Engine Research Building (ERB)
The ERB is the largest and most adaptable test facility complex at Glenn, with 152,235 square feet of floor space housing more than 60 test rigs.
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Flight Research Building (Hangar)
Built in the 1940's, the Hangar is a 65 X 250 ft. heated facility that is large enough to hold numerous aircraft of various sizes.
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Heated Tube Facility
The Heated Tube Facility investigates cooling issues by simulating conditions characteristic of thrust chambers and propulsion systems.
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Hypersonic Tunnel Facility (HTF)
The Heated Tube Facility investigates cooling issues by simulating conditions characteristic of thrust chambers and propulsion systems.
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Icing Research Tunnel (IRT)
The IRT provides a true icing environment for testing and certification of aircraft components.
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Power Systems Facility (PSF)
PSF houses testbeds to verfiy criticial design concepts under actual loading and operating conditions.
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Propulsion Systems Laboratory (PSL)
The PSL is NASA's only ground-based test facility that can provide true flight simulation for research on air-breathing propulsion systems.
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Research Combustion Laboratory (RCL)
The RCL develops aerospace propulsion technology by performing tests on propulsion components and materials.
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Small Multi-Purpose Research Facility (SMiRF)
The SMiRF, part of the RCL, evaluates the thermal protection systems required to provide long-term storage of cryogenic propellants in space.
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Space Power Facility (SPF)
The Space Power Facility (SPF) houses the world's largest space environment simulation chamber.
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Structural Dynamics Laboratory (SDL)
The SDL performs tests to verify the survivability of a component or assembly when exposed to vibration and environmental stress.
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Zero Gravity Research Facility (Zero-G)
The Zero Gravity Research Facility is NASA’s premier facility for ground based microgravity research, and the largest facility of its kind in the World.
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