00.60 Apr 10, 2024
ISO
ISO/TC 20/SC 16
International Standard
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.
IN_DEVELOPMENT
ISO/PWI 24222
00.60
Close of review
Apr 10, 2024
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