GB/T 38930-2020 Active
GB/T 38930-2020 Requirements and test methods of the capability of wind resistance for civil small and light unmanned aircraft system
Abstract
This standard specifies the wind resistance requirements and test methods for civil small unmanned aerial vehicle systems, including wind resistance requirements, test purposes, test conditions, test environment, test interruption and recovery, test criteria, test process, test data processing, test result evaluation, and test reports. This standard applies to civil small rotary-wing UAV systems (with a takeoff weight of between 0.25 kg and 150 kg), including unmanned helicopter systems, multi-rotor UAV systems, vertical takeoff and landing fixed-wing UAV systems (during the takeoff and landing phases only), and other rotary-wing UAV systems; other types of UAV systems may refer to this standard for implementation.
General Product Information
| Document Type | National standards |
|---|---|
| Standard Status | Active |
| Standard Code | GB/T 38930-2020 |
| CCS | Aircraft and their accessories |
| ICS | Integrated aircraft and spacecraft |
| Implement Date | 2021-02-01 |