Design of a Tube Launched Man Portable Unmanned Aerial Vehicle

Date

2007-03-29T12:49:08Z

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Department

Department of Aerospace, Power and Sensors

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Thesis or dissertation

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Abstract

The aim of the MSc was to design a man portable tube launched Unmanned Aerial Vehicle (UAV). The resulting UAV has a vertically staggered wing layout and a V-tail. The UAV has folding wings and tail to allow the deployment from a tube and is small in size to allow it to be man portable. Several design variants were experimented with to verify the staggered wing configuration. The outcome is that a small UAV suitable for tube launching is possible, although the UAV has yet to be launched from a tube.

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Github

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© Cranfield University 2006. All rights reserved. No part of this publication may be reproduced without the prior permission of the copyright owner.

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