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: Apr 10, 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
Apr 10, 2024

Preview

Only informative sections of projects are publicly available. To view the full content, you will need to members of the committee. If you are a member, please log in to your account by clicking on the "Log in" button.