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Technical Committee No |
TC02 |
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Status |
Active |
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Category |
Mechanical Sector |
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Sub Category |
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$Resources:StandardType; |
Kuwaiti Standard |
This document specifies the procedures for testing flight stability of a multi-copter unmanned aircraft system (UAS) and is applicable to multi-copter type UAS that can take-off and land vertically. A commercial multi-copter UAS weighing over 250 g to less than 150 kg is discussed in this document. Further, this document is applicable to military and civilian multi-copter UAS. However, quantitatively specific stability criteria for the test are not specified in this document.
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Decision No |
51/2025 |
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Decision By |
From Ministers Office |
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Date of Meeting |
13-08-2025 |
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Approval Date |
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Decision Date |
12-11-2025 |
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Newspaper Publication Date |
07-12-2025 |
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Newspaper Number |
1768 |
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