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Flight performance of civil small and light fixed-wing unmanned aircraft systems (UAS) — Test methods
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STANDARD published on 23.10.2023
Designation standards: ISO 5286:2023
Publication date standards: 23.10.2023
SKU: NS-1158164
The number of pages: 8
Approximate weight : 24 g (0.05 lbs)
Country: International technical standard
Category: Technical standards ISO
Description / 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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Latest update: 2026-01-26 (Number of items: 2 257 479)
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