GB/T 38924.6-2020 Active
GB/T 38924.6-2020 Environmental test methods for civil small and light unmanned aircraft system—Part 6:Vibration test
Abstract
This part of GB/T 38924 specifies the vibration test requirements and methods for civilian lightweight and small unmanned aerial vehicles (with a takeoff weight of 0.25 kg to 150 kg), including test conditions, test equipment and instruments, test process, test interruption and resumption, test result evaluation, and test reports, etc.
This part is applicable to civilian lightweight and small (with a maximum takeoff weight of more than 0.25 kg and not more than 150 kg) multi-rotor UAV systems, fixed-wing UAV systems, unmanned helicopter systems, and vehicle-mounted ground stations that may experience vibration environments during transportation and use, in order to determine whether civilian lightweight and small UAV systems can withstand the effects of vibration environments.
General Product Information
| Document Type | National standards |
|---|---|
| Standard Status | Active |
| Standard Code | GB/T 38924.6-2020 |
| CCS | Aircraft and their accessories |
| ICS | Integrated aircraft and spacecraft |
| Implement Date | 2021-02-01 |