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Parachute recovery for UAV systems

Tim Wyllie (Tim Wyllie is Senior Systems Engineer, based at Future Systems Technology Division, DERA Farnborough, Farnborough, UK.)

Aircraft Engineering and Aerospace Technology

ISSN: 0002-2667

Article publication date: 1 December 2001

2576

Abstract

Parachute recovery systems are described from a systems perspective. Parachute recovery is particularly suited to tactical fixed wing UAV systems that require a high degree of mobility by allowing air vehicle recovery onto unprepared terrain. The descent environment is described, and the impact of wind on recovery is considered. The relative merits of cruciform, round and parafoil canopies are assessed, taking three real‐world systems as design examples. Throughout, design considerations are approached from a systems perspective, with a view to producing safe, autonomous and accurate recovery systems.

Keywords

Citation

Wyllie, T. (2001), "Parachute recovery for UAV systems", Aircraft Engineering and Aerospace Technology, Vol. 73 No. 6, pp. 542-551. https://doi.org/10.1108/00022660110696696

Publisher

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MCB UP Ltd

Copyright © 2001, Government agency

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