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