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Rocket turbine engine

From Wikipedia, the free encyclopedia

Arocket turbine engine is a combination of two types of propulsion engines: aliquid-propellant rocket and a turbinejet engine. Itspower-to-weight ratio is a little higher than a regular jet engine, and works at higher altitudes.^[1]^[2]^[3]

^"Analysis of the effect of factors on the efficiency of liquid rocket turbine" by Zu, Guojun; Zhang, YuanjunJournal of Propulsion Technology no. 6, p. 38-43, 58.[1]
^ Hydrogen peroxide based propulsion system for micro air vehicle applications b WS Cheung, JR Tilston ISABE 99-7298"Hydrogen Peroxide Based Propulsion System for Micro Air Vehicle Applications"(PDF). Archived fromthe original(PDF) on 2011-07-11. Retrieved2011-03-10.
^Cheung, W. S.; Tilston, J. R. (2001)."Testing of a novel propulsion system for micro air vehicles".Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering.215 (4):207–218.doi:10.1243/0954410011533194.S2CID 110935499. RetrievedApril 8, 2023.