IEC - 62282-4-202
Fuel cell technologies – Part 4-202: Fuel cell power systems for propulsion and auxiliary power units – Unmanned aircrafts – Performance test methods
| Organization: | IEC |
| Publication Date: | 1 October 2023 |
| Status: | active |
| Page Count: | 46 |
| ICS Code (Fuel cells): | 27.070 |
| ICS Code (Aircraft and space vehicles in general): | 49.020 |
scope:
This part of IEC 62282 covers performance test methods of fuel cell power systems intended to be used to power unmanned aircrafts, including general requirements, start-up, shutdown, power output, continuous running time, electric efficiency, data transmission, warning and monitoring, environmental compatibility, etc.
The scope of this document is limited to electrically powered unmanned aircrafts with a maximum take-off mass not exceeding 150 kg (i.e. level 5 or lower unmanned aircrafts (UAs)).
This document applies to fuel cell power systems with a rated output voltage not exceeding 220 V DC for outdoor use.
This document applies only to compressed gaseous hydrogen-fuelled fuel cell power systems.
This document does not apply to reformer-equipped fuel cell power systems.
Document History
