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

  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.
  2. ↑ Hydrogen peroxide based propulsion system for micro air vehicle applications b WS Cheung, JR Tilston ISABE 99-7298
  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


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