IEC 62282-4-202:2023
Current
The latest, up-to-date edition.
Fuel cell technologies - Part 4-202: Fuel cell power systems for propulsion and auxiliary power units - Unmanned aircrafts - Performance test methods
Hardcopy , PDF
English - French
17-10-2023
IEC 62282-4-202:2023 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.
| Committee |
TC 105
|
| DocumentType |
Standard
|
| Pages |
41
|
| PublisherName |
International Electrotechnical Committee
|
| Status |
Current
|
| Standards | Relationship |
| I.S. EN IEC 62282-4-202:2023 | Equivalent |
| BS EN IEC 62282-4-202:2023 | Equivalent |
| UNE-EN IEC 62282-4-202:2023 | Equivalent |
| DIN EN IEC 62282-4-202:2024-07 | Identical |
| CEI EN IEC 62282-4-202:2024-06 | Identical |
| VDE 0130-4-202:2024-07 | Identical |
| UNE-EN IEC 62282-4-202:2023 | Identical |
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