ISO 5286:2023
p
ISO 5286:2023
81110

Status : Published

en
Format Language
std 1 63 PDF + ePub
std 2 63 Paper
  • CHF63
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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.

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General information

  •  : Published
     : 2023-10
    : International Standard published [60.60]
  •  : 1
     : 8
  • ISO/TC 20/SC 16
    49.020 
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