Design of a Tube Launched Man Portable Unmanned Aerial Vehicle

dc.contributor.advisorKnowles, Kevin
dc.contributor.advisorBray, Derek
dc.contributor.authorProctor, S
dc.date.accessioned2007-03-29T12:49:08Z
dc.date.available2007-03-29T12:49:08Z
dc.date.issued2007-03-29T12:49:08Z
dc.description.abstractThe 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.en
dc.format.extent21910016 bytes
dc.format.mimetypeapplication/msword
dc.identifier.urihttp://hdl.handle.net/1826/1531
dc.language.isoenen
dc.publisher.departmentDepartment of Aerospace, Power and Sensorsen
dc.rights© Cranfield University 2006. All rights reserved. No part of this publication may be reproduced without the prior permission of the copyright owner.en
dc.titleDesign of a Tube Launched Man Portable Unmanned Aerial Vehicleen
dc.typeThesis or dissertationen
dc.type.qualificationlevelMastersen
dc.type.qualificationnameMScen

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