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IEC 62282-4-202:2023 PDF

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

First page of standard IEC 62282-4-202:2023Open preview (PDF)Fuel cell technologies - Part 4-202: Fuel cell power systems for propulsion and auxiliary power units - Unmanned aircrafts - Performance test methods
Title (English):
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

Document status:
Active
Format:
Electronic (PDF)
Number of pages:
41
Publication date:
October 17, 2023
Edition:
IEC IS 62282 edition 1 version 1
ICS:
27.070
Description (English):

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.

Technical details

Technical committee
TC 105 - Fuel cell technologies
SKU
IEC 62282-4-202:2023

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