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ISO/PWI 24222

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

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00.60     10. 4. 2024.

ISO

ISO/TC 20/SC 16

Međunarodni standard

Apstrakt

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.

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TRENUTNO

PROJEKAT
ISO/PWI 24222
00.60 Donošenje odluke o predlogu novog projekta
10. 4. 2024.