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ASTM F2585-06
Standard Specification for Design and Performance of Pneumatic-Hydraulic Unmanned Aircraft System (UAS) Launch System
STANDARD published on 1.12.2006
The information about the standard:
Designation standards: ASTM F2585-06
Note: WITHDRAWN
Publication date standards: 1.12.2006
SKU: NS-54184
The number of pages: 7
Approximate weight : 21 g (0.05 lbs)
Country: American technical standard
Category: Technical standards ASTM
Annotation of standard text ASTM F2585-06 :
Keywords:
catapult, launch, take-off, UA, UAS, unmanned aircraft system, ICS Number Code 49.020 (Aircraft and space vehicles in general)
Additional information
| 1. Scope | ||
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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. |
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| 2. Referenced Documents | ||
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