Status : Published
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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.

General information

  • Status
     : Published
    Publication date
     : 2023-10
    Stage
    : International Standard published [60.60]
  • Edition
     : 1
    Number of pages
     : 8
  • Technical Committee :
    ISO/TC 20/SC 16
    ICS :
    49.020 
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Life cycle

Sustainable Development Goals

This standard contributes to the following Sustainable Development Goal

9
Industry, Innovation and Infrastructure

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