prBAS EN IEC 62282-4-202:2025
Fuel cell technologies - Part 4-202: Fuel cell power systems for propulsion and auxiliary power units - Unmanned aircrafts - Performance test methods
General information
Status:Project
Number of pages:45
Adoption method:Proglašavanje
Language:engleski,francuski
Edition:1.
Realization date:17.12.2024
Forseen date for next stage code:23.12.2024
Technical committee:BAS/TC 56, Conventional and alternative sources of electrical energy
ICS:
49.020, Aircraft and space vehicles in general
27.070, Fuel cells
27.070, Fuel cells
Abstract
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.
Lifecycle
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Original document and degree of correspondence
EN IEC 62282-4-202:2023, identical
IEC 62282-4-202:2023, identical
Work material
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