Flight performance of civil small and light fixed-wing unmanned aircraft systems (UAS) — Test methods
NORM herausgegeben am 23.10.2023
Designation standards: ISO 5286:2023
Publication date standards: 23.10.2023
The number of pages: 8
Approximate weight : 24 g (0.05 lbs)
Country: International technical standard
Kategorie: Technische Normen ISO
Description / Abstract: 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.