BS EN IEC 62282-4-202:2023
Current
The latest, up-to-date edition.
Fuel cell technologies Fuel cell power systems for propulsion and auxiliary power units. Unmanned aircrafts. Performance test methods
Hardcopy , PDF
English
08-12-2023
| Committee |
GEL/105
|
| DocumentType |
Standard
|
| Pages |
26
|
| PublisherName |
British Standards Institution
|
| Status |
Current
|
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.
| Standards | Relationship |
| I.S. EN IEC 62282-4-202:2023 | Equivalent |
| IEC 62282-4-202:2023 | Equivalent |
| UNE-EN IEC 62282-4-202:2023 | Equivalent |
| EN IEC 62282-4-202:2023 | Equivalent |
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