ASTM-F2585 › Historical Revision Information
Standard Specification for Design and Performance of Pneumatic-Hydraulic Unmanned Aircraft System (UAS) Launch System (Withdrawn 2017)
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Scope
1.1 This specification covers the design and performance of unmanned aircraft system (UAS) launch system operating via a closed-loop pressurized hydraulic or pneumatic system with a hydraulic recovery, or both.
1.2 In instances where the launcher and UAS manufacturer are the same entity, compliance with this specification is the responsibility of the UAS manufacturer where applicable.
This standard does not purport to address all of the safety concerns, if any, associated with its use. It is the responsibility of the user of this standard to establish appropriate safety and health practices and determine the applicability of regulatory limitations prior to use.
Keywords
catapult; launch; take-off; UA; UAS; unmanned aircraft system; ICS Number Code 49.020 (Aircraft and space vehicles in general)
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Document Number
ASTM-F2585
Revision Level
WITHDRAWN
Status
Cancelled
Modification Type
New
Publication Date
July 15, 2017
Document Type
Specification
Committee Number
F38.01