Wing Support Structure LSU03 UAV Strengthen for Dynamic Load

Atik Bintoro (2016) Wing Support Structure LSU03 UAV Strengthen for Dynamic Load. Proceedings International Seminar on Aerospace Science and Technology (ISAST) 2016. pp. 1-11.

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LSU03 UAV was resulted by Aeronautics Technology Center, National Institute of Aeronautics and Space, LAPAN. This UAV has flight scenario like small UAV comprising taxi moves, take off, cruising, descending and landing. The operational of this craft was appeared stress structure specially wing support structure. The appearing of this stress was caused by the dynamic load or shock loads which the biggest at early landing and first touchdown in ground plane. With the dimensional data of wing support structure, analytical method, mission objective research and flight operational of LSU03 can be known that the structure can fulfill mission that is robust, light and strength. E-glass composite material was used as material of the wing support structure. This structure is strengthen receive dynamic load during flight time and landing.

Item Type: Article
Additional Information: ISBN 978-602-6465-03-0
Uncontrolled Keywords: dynamic load, e-glass, LSU03 UAV, wing, landing
Subjects: Teknologi Penerbangan dan Antariksa > Penelitian, Pengembangan, Perekayasaan, dan Pemanfaatan > Teknologi Aeronautika
Divisions: Deputi Teknologi Penerbangan Dan Antariksa > Pusat Teknologi Penerbangan
Depositing User: Dinar Indrasasi
Date Deposited: 28 Sep 2021 00:03
Last Modified: 30 Sep 2021 00:23

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