ISO/PWI 24222

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

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.