ISO/PWI 24222

Civil small and light unmanned aircraft systems (UAS) under high-temperature and low-temperature conditions — Test methods

General information

Current stage: 00.60 Effective date: 10 pri 2024

Originator: ISO

Owner: ISO/TC 20/SC 16

Type: International Standard

Scope

This document mainly specifies the test conditions, apparatus, procedure and evaluation methods to be used for the high-temperature and low-temperature testing of unmanned aircraft system (UAS) with maximum take-off mass (MTOM) between 250 g and 25 kg, in order to determine the adaptability to harsh temperature environments.

Life cycle

NOW

IN_DEVELOPMENT
ISO/PWI 24222
00.60 Close of review
10 pri 2024

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