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Design of a Tube Launched Man Portable Unmanned Aerial Vehicle

By S Proctor

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

Publisher: Department of Aerospace, Power and Sensors
Year: 2007
OAI identifier: oai:dspace.lib.cranfield.ac.uk:1826/1531
Provided by: Cranfield CERES
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