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 work 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 [2]
- ^ "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 [3]
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