Hübriidrakettide
Hübriidrakettide is a term that generally refers to hybrid rocket engines. These engines combine aspects of both solid-fuel and liquid-fuel rocket engines. The most common configuration involves a solid fuel grain and a liquid or gaseous oxidizer. The solid fuel, typically a rubber-like material, is cast into a combustion chamber. The oxidizer is then injected into the chamber, where it vaporizes and mixes with the burning fuel. Combustion occurs on the surface of the solid fuel grain.
The primary advantage of hybrid rockets lies in their relative simplicity and safety compared to traditional
However, hybrid rockets also face challenges. Achieving high performance, comparable to liquid-fuel engines, can be difficult