This standard provides comprehensive testing and acceptance technical guidance for hydrogen cylinder valves of unmanned aircraft systems (UASs) in low-temperature environments for UAS users, hydrogen cylinder manufacturers, valve manufacturers, and other enterprises. It elaborates on relevant terms, definitions, technical requirements, test methods, and evaluation criteria, and is applicable to the verification of hydrogen cylinder valves of UASs in ambient temperatures ranging from –50 °C to –10 °C.
- Standard Committee
- COM/AerCom-SC - Unmanned Aerial Vehicles Communications Standards Committee
- Status
- Active PAR
- PAR Approval
- 2025-06-19
Working Group Details
- Society
- IEEE Communications Society
- Standard Committee
- COM/AerCom-SC - Unmanned Aerial Vehicles Communications Standards Committee
- Working Group
-
TTHCV - Technical Requirements and Testing Methods for Hydrogen Cylinders Valves of Unmanned Aircraft Systems in Low-Temperature Environments
- IEEE Program Manager
- Michael Kipness
Contact Michael Kipness - Working Group Chair
- Wang Lei
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