Application Type
Organization
Scope
This standard specifies the general, technical, test and inspection, label, packaging and transport requirements for fuel cell power systems for UAV.
This standard is applicable to fuel cell power systems that use compressed hydrogen as fuel to provide power and non-drive power for UAVs with an unloaded weight of no more than 116 kg and a maximum takeoff weight of not more than 150 kg.
Status
Status Explanation
Recently ratified, but not yet released.