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 "Archived copy" (PDF). Archived from the original (PDF) on 2011-07-11. Retrieved 2011-03-10.
{{cite web}}: 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]
 | This technology-related article is a stub. You can help Wikipedia by expanding it. |
 | This rocketry article is a stub. You can help Wikipedia by expanding it. |
 | This aviation-related article is a stub. You can help Wikipedia by expanding it. |