Rocket turbine engine

A rocket turbine engine is a combination of two types of propulsion engines: a liquid fuel 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 "Archived copy" (PDF). Archived from the original (PDF) on 2011-07-11. Retrieved 2011-03-10.CS1 maint: archived copy as title (link)
^ "Testing of a novel propulsion system for micro air vehicles" Pfoceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering" Volume 215, Number 4, pages 207-218 / 2001 [2]^{[permanent dead link]}

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[1] "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]

[2] Hydrogen peroxide based propulsion system for micro air vehicle applications b WS Cheung, JR Tilston ISABE 99-7298 "Archived copy" (PDF). Archived from the original (PDF) on 2011-07-11. Retrieved 2011-03-10.CS1 maint: archived copy as title (link)

[3] "Testing of a novel propulsion system for micro air vehicles" Pfoceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering" Volume 215, Number 4, pages 207-218 / 2001 [2]^{[permanent dead link]}

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