ISO 5312:2023
Civil small and light unmanned aircraft (UA) — Sharp injury to human body by rotor blades — Evaluation and test method
Product Details
This document is applicable to evaluating and testing the sharp injury to human body caused by rotor blades of civil small and light UA (with maximum take-off mass between 0,25 kg to 4 kg, which are between the levels II and III as categorized by ISO 21895), including multicopter UA, unmanned helicopters and other rotor UA.