00.60 10. 4. 2024.
ISO
ISO/TC 20/SC 16
Међународни стандард
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.
ПРОЈЕКАТ
ISO/PWI 24222
00.60
Доношење одлуке о предлогу новог пројекта
10. 4. 2024.