ISO 5286:2023

Flight performance of civil small and light fixed-wing unmanned aircraft systems (UAS) — Test methods

OVERVIEW

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.

COMMENTS

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PRODUCT DETAILS

Status Current
Edition 2023
No. of Pages 8
ICS Classification 49.020 Aircraft and space vehicles in general
Committee ISO/TC 20/SC 16
Available for Purchase For sale in Singapore only
Adoption ISO : 0