UNE-EN IEC 62282-4-202:2023
Current
Fuel cell technologies - Part 4-202: Fuel cell power systems for propulsion and auxiliary power units - Unmanned aircrafts - Performance test methods (Endorsed by Asociación Española de Normalización in January of 2024.)
Hardcopy , PDF
English
01-01-2024
This document covers performance test methods of fuel cell power systems intended for being 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 the document is limited to electric powered unmanned aircrafts with a maximum take-off mass not exceeding 150 kg (i.e., level 5 or lower UAs). The document applies to fuel cell power systems with a rated output voltage not exceeding 220 V DC for outdoor use. The document applies only to compressed gaseous hydrogen-fuelled fuel cell power systems. The document does not apply to reformer-equipped fuel cell power systems.
| Committee |
CTN 222
|
| DocumentType |
Standard
|
| Pages |
29
|
| PublisherName |
Asociación Española de Normalización
|
| Status |
Current
|
| Standards | Relationship |
| I.S. EN IEC 62282-4-202:2023 | Equivalent |
| BS EN IEC 62282-4-202:2023 | Equivalent |
| EN IEC 62282-4-202:2023 | Identical |
| IEC 62282-4-202:2023 | Identical |
| IEC 62282-4-202:2023 | Equivalent |
| EN IEC 62282-4-202:2023 | Equivalent |
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