ISO-5286 › Flight performance of civil small and light fixed-wing unmanned aircraft systems (UAS) - Test methods

ISO-5286 - 1ST EDITION - CURRENT


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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.

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49.020 (Aircraft and space vehicles in general Including aircraft performance, flight dynamics, etc. Air transport, see 03.220.50)

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Document Number

ISO 5286:2023

Revision Level

1ST EDITION

Status

Current

Publication Date

Oct. 1, 2023

Committee Number

ISO/TC 20/SC 16