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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.
Reģistrācijas numurs (WIID)
87781
Darbības sfēra
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.
