GB/T 38924.5-2020 Environmental test methods for civil small and light unmanned aircraft system—Part 5:Shock test

Scope

This part of GB/T 38924 specifies the impact test requirements and methods for civil lightweight and small unmanned aerial vehicles (with a takeoff weight of 0.25 kg to 150 kg) systems (including aircraft and ground stations), including test conditions, test equipment and instruments, test process, test interruption and resumption, test result evaluation, and test reports.
This part is applicable to civil lightweight and small unmanned aerial vehicles (with a takeoff weight of 0.25 kg to 150 kg) systems (including aircraft and ground stations) that may experience impact environments during transportation, loading, and use, in order to determine whether these civil lightweight and small unmanned aerial vehicles can withstand the effects of impact environments.

Development Information

Same series standard

Referenced Standards

Related Standards