Design of a Tube Launched Man Portable Unmanned Aerial Vehicle
dc.contributor.advisor | Knowles, Kevin | |
dc.contributor.advisor | Bray, Derek | |
dc.contributor.author | Proctor, S | |
dc.date.accessioned | 2007-03-29T12:49:08Z | |
dc.date.available | 2007-03-29T12:49:08Z | |
dc.date.issued | 2007-03-29T12:49:08Z | |
dc.description.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. | en |
dc.format.extent | 21910016 bytes | |
dc.format.mimetype | application/msword | |
dc.identifier.uri | http://hdl.handle.net/1826/1531 | |
dc.language.iso | en | en |
dc.publisher.department | Department of Aerospace, Power and Sensors | en |
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.title | Design of a Tube Launched Man Portable Unmanned Aerial Vehicle | en |
dc.type | Thesis or dissertation | en |
dc.type.qualificationlevel | Masters | en |
dc.type.qualificationname | MSc | en |