Test Technology: Temperature Measurement
Temperature measurements are necessary to develop the design characteristics that are needed for vehicle heating (surface or internal), and to maintain correct air flow conditions.
Focus Areas and Capabilities
Learn more about the specifications and capabilities of this facility.
Quick Facts
The 9'x15' Low Speed Wind Tunnel provides customers with a facility capable of testing large scale aeropropulsion hardware.
Techniques
These techniques address different types of instrumentation for carrying out pressure measurements.
Capabilities
Different forms of information may come from known measurement techniques.
Test Technology: Temperature Measurement Gallery
AETC Test Technologies
Test Technology supports ATP by keeping NASA’s research test facilities and flight assets moving into the future.
As the world’s technologies continue to improve and research requirements become more demanding, Test Technology provides new and improved capabilities for measuring pressure, temperature, angle, strain, and air flow.
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AETC Ground Facilities
AETC sets the strategic direction for NASA’s versatile and comprehensive portfolio of ground test aeronautics research capabilities.
Among these assets are subsonic, transonic, supersonic, and hypersonic wind tunnels and propulsion test facilities at Ames Research Center, Glenn Research Center, and Langley Research Center.
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AETC
Aerosciences Evaluation and Test Capabilities (AETC) Portfolio Office
The AETC Portfolio Office executes strategic efforts to preserve and enhance research and test capabilities for NASA’s world-class portfolio of National Wind Tunnel facilities.
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