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ISO 5286:2023

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

Summary

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.

Notes

60.60 : Norme internationale publiée

Technical characteristics

Publisher International Organization for Standardization (ISO)
Publication Date 10/23/2023
Edition 1
Page Count 8
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ISBN ---
Weight (in grams) ---
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