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All-optical method of determining liquid level in cryogenic liquid

Completed TRL 4 (started at 2, targeting 4)

Description

design minimum fuel supersonic flight test trajectories using modern software tools & techniques. Validate fuel burn predictions with real-world F-18 flight test. Transition workflow to X-59.

Benefits

Distinguish between ullage and liquid level of flammable cryogen without needing electric current, benefit in future lunar ISRU of fuel liquefaction.

Details

Technology areaSensors and Instruments > In Situ Instruments and Sensors > Environment Sensors
ProgramCenter Innovation Fund: AFRC CIF (AFRC CIF)
Lead organizationArmstrong Flight Research Center, Edwards, CA
Start date2021-10-01
End date2022-09-30

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