Standard

SFS-EN IEC 62282-4-202:2023

Dec 2023 Published

Corrigendums and amendments are bought separately.

Language English

Services Read online + Print/Download €169.00 Read online €138.00 Printed and bound Delivery time: 5-10 days €169.00 Read online + Copy/paste €169.00

There are no extended editions available for this standard

There are no available corrigendum or amendments for this standard. Any future corrigendum and amendments will be added automatically for subscribers.

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.

Document information

Standard from SFS-sähkö
Published: 15 December 2023
Edition: 1
Document type: IS
Pages
ISBN:

Publisher SFS
Distributor SFS-sähkö
Technical Committee CLC/SR 105

SFS-EN IEC 62282-4-202:2023

Create subscription

Benefits of a subscription:

Abstract

Document information

Create subscription

Benefits of a subscription:

Extended editions Extended editions (0)

Version history Related corrigendum and amendments (0)

Abstract

Document information