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ASTM F2585-06
Standard Specification for Design and Performance of Pneumatic-Hydraulic Unmanned Aircraft System (UAS) Launch System
7 стр.
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93.60 $ (включая НДС 20%)
Разработчик:
Зарубежные/ASTM
ICS:
49.020 Aircraft. Including aircraft performance, flight dynamics, etc. / Авиационные и космические аппараты в целом. Включая эксплуатацию самолетов, динамику полетов и т.д.
Сборник (ASTM):
15.09 Light Sport Aircraft; Unmanned Aircraft Systems; Aircraft Systems; Aerospace Personnel; General Aviation Aircraft / Легкие спортивные летательные аппараты; Беспилотные летательные системы; Летательные системы; Аэрокосмический персонал; Авиация общего назначения
Тематика:
Aerospace Materials
Описание
Область применения

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.

Ключевые слова:
catapult; launch; take-off; UA; UAS; unmanned aircraft system