Full Description

This document specifies the test requirements and methods for verifying the specified flight performance items of civil fixed-wing unmanned aircraft systems (UAS).

This document is applicable to the category of civil small and light fixed-wing UAS, which applies to maximum take-off mass (MTOM) level I through V according to ISO 21895.

Product Details

Published: 10/01/2023 File Size: 1 file , 1000 KB Note: This product is unavailable in Ukraine, Russia, Belarus