Turbo Solutions engineers have been designing and analyzing aircraft propulsion systems since 1988. Recent projects have included turbocompression systems for medium- and high-altitude unmanned aerial vehicles (UAVs), aerodynamic design and analysis of compressors and turbines for an air turbo-rocket (ATR), comprehensive thermal analysis of a small jet engine, and cycle design and analysis for turbocharged diesel aircraft propulsion systems. Past programs include the development of an integrated health management system for rocket turbopumps, the design of a high specific speed inducer for a liquid oxygen (LOX) turbopump, and the design of LOX and methane turbopumps for a medium-thrust expander cycle rocket engine. Turbo Solutions can either start with initial specifications to produce a clean-sheet propulsion system design all the way through prototype manufacturing and testing, or we can analyze and then redesign an existing machine, providing improved performance, reduced cost, and extended component and system life. Our decades of experience in the design, analysis, fabrication, and testing of aerospace propulsion systems enables us to deliver systems or components that meet your performance, life, and cost demands.
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