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ISO 5286:2023

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

Standard Details

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.

General Information

Status : Published
Standard Type: Main
Document No: ISO 5286:2023
Document Year: 2023
Pages: 8
Edition: 1
  • ICS:
  • 49.020 Aircraft and space vehicles in general

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ISO 5286:2023
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