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EN IEC 62282-4-202:2023

Fuel cell technologies - Part 4-202: Fuel cell power systems for propulsion and auxiliary power units - Unmanned aircrafts - Performance test methods EN IEC 62282-4-202:2023

Publication date:   Feb 19, 2024

General information

60.60 Standard published   Dec 1, 2023

CENELEC

CLC/SR 105 Fuel cell technologies

European Norm

27.070   Fuel cells | 49.020   Aircraft and space vehicles in general

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Scope

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.

Life cycle

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PUBLISHED
EN IEC 62282-4-202:2023
60.60 Standard published
Dec 1, 2023