ASTM F 2585 : 2008
Withdrawn
A Withdrawn Standard is one, which is removed from sale, and its unique number can no longer be used. The Standard can be withdrawn and not replaced, or it can be withdrawn and replaced by a Standard with a different number.
Standard Specification for Design and Performance of Pneumatic-Hydraulic Unmanned Aircraft System (UAS) Launch System (Withdrawn 2017)
Hardcopy , PDF
14-07-2017
English
01-08-2008
Important note : Users cannot be edited or removed once added to your Multi user PDF.| Committee |
F 38
|
| DocumentType |
Standard
|
| Pages |
7
|
| PublisherName |
American Society for Testing and Materials
|
| Status |
Withdrawn
|
| Supersedes |
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.
1.3 This standard does not purport to address all of the safety concerns associated with the USA launch system and 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.
| ASTM F 2911 : 2014 : EDT 1 | Standard Practice for Production Acceptance of Small Unmanned Aircraft System (sUAS) (Withdrawn 2023) |
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