ISO/PWI 24222

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

General information

00.60 Close of review   Apr 10, 2024

ISO

ISO/TC 20/SC 16 Unmanned aircraft systems

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