Rocket turbine engine

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

References

^ "Analysis of the effect of factors on the efficiency of liquid rocket turbine" by Zu, Guojun; Zhang, Yuanjun Journal 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 from the original (PDF) on 2011-07-11. Retrieved 2011-03-10.

^ 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. Retrieved April 8, 2023.

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