This standard specifies technical requirements, testing methods, and application specifications for Hydrogen-Powered Unmanned Aerial System (UAS). It covers three key technical areas: Hydrogen-powered cell materials, Hydrogen-powered technology equipment, and multi-rotor UAS integration, including core technical indicators such as material properties, hydrogen storage systems, refueling facilities, flight performance, and safety monitoring. The standard sets performance requirements for hydrogen-powered multi-rotor UAS, including environmental adaptability, dynamic response, and energy conversion efficiency, while standardizing technical parameters for three hydrogen storage methods: high-pressure gaseous, liquid, and solid-state hydrogen storage. It also clarifies implementation requirements for hydrogen refueling station construction, data monitoring, and typical application scenarios, providing a technical basis for the safe application of hydrogen-powered UAS in fields such as agriculture, power line inspection, and island operations.
- Standard Committee
- COM/AerCom-SC - Unmanned Aerial Vehicles Communications Standards Committee
- Status
- Active PAR
- PAR Approval
- 2025-05-28
Working Group Details
- Society
- IEEE Communications Society
- Standard Committee
- COM/AerCom-SC - Unmanned Aerial Vehicles Communications Standards Committee
- Working Group
-
P1958 HFCWG - P1958 WG Hydrogen Fuel Cell Application Framework on Multi-rotor Drones
- IEEE Program Manager
- Michael Kipness
Contact Michael Kipness - Working Group Chair
- Lei YAN
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