Stepped piston engines for multi-fuel UAV application
Stepped piston engines for multi-fuel UAV application
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Date
2005-04-14
Authors
Hooper, P
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Item type
Conference Contribution
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Publisher
Institution of Mechanical Engineers (IMechE)
Abstract
This paper presents design and development data for the SPV580 Unmanned Air Vehicle (UAV) engine. The project was funded by the British Ministry of Defence to meet future need for low mass power plants for advanced UAVs. Development has investigated gasoline and heavy fuelling, and data is presented on the achievements to date, together with predictive data if more advanced fuel system technology is applied. Summary data from a further study to provide higher power output from low mass stepped piston engines is also presented.
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Source
IMechE Conference on Propulsion Systems for Unmanned Aircraft held at BAWA, Bristol, UK, 2005-04-14 to 2005-04-14
DOI
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NOTICE: this is the author’s version of a work that was accepted for publication. Changes resulting from the publishing process, such as peer review, editing, corrections, structural formatting, and other quality control mechanisms may not be reflected in this document. Changes may have been made to this work since it was submitted for publication. A definitive version was subsequently published in (see Citation).