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ASTM F2585-06

Historical Revision

Standard Specification for Design and Performance of Pneumatic-Hydraulic Unmanned Aircraft System (UAS) Launch System (Withdrawn 2017)

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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.


SDO ASTM: ASTM International
Document Number F2585
Publication Date Dec. 1, 2006
Language en - English
Page Count 7
Revision Level 06
Supercedes
Committee F38.01
Publish Date Document Id Type View
Aug. 1, 2008 F2585-08 Revision
Dec. 1, 2006 F2585-06 Revision