NASA HIGH SPEED VEHICLE TECHNOLOGY DEVELOPMENT WOULD REQUIRE ROBUST AND RELIABLE PRESSURE AND TEMPERATURE SENSORS THAT WOULD SUPPORT GROUND AND FLIGHT EXPERIMENTAL TEST CAMPAIGNS. THESE SENSORS WOULD VALIDATE THE COMPUTATIONAL FLUID DYNAMICS CODES TH
Start Date: Sep 4, 2025
End Date: Sep 3, 2029
13% of period elapsed
Awarding Agency
NANATIONAL AERONAUTICS AND SPACE ADMINISTRATION
Code: 8000
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