Hybrid Rocket Engine
Developing Phoenix, a small hybrid rocket engine with variable thrust and precise vectoring capabilities
How It All Started
Fascination with aerospace and inspiration from friends spurred me to begin experimenting with building my own rocket engines. The Journey began with the review of textbooks like Rocket Propulsion Elements and the creation of some preliminary sketches.
The Vision
Using ABS plastic for fuel and Liquid Nitrous Oxide as its oxidizer, the goal was to create a compact hybrid rocket engine capable of variable thrust and precise vectoring. Designed for performance and efficiency, it is estimated that Phoenix will produce approximately 1100N of thrust for 7s
Variable Thrust and Vectoring
Thrust vectoring is the process of manipulating the direction of an engine's thrust to steer a rocket's flight path, while variable thrust refers to the adjustment of the engine's power output to control the speed and altitude.
Whats Next?
I am now preparing to assemble the engine and gear up for the first test fire. If successful, this will validate my design and serve as a stepping stone for more complex rocketry endeavors.
Project Release
Completion of this project is on the horizon. Expect this page to be updated with comprehensive details soon.