Term 242

Synergizing Propulsion Systems: Enhancing Hybrid Rocket Performance through Altitude Optimized Integ

Project Type: Self-Initiated

Project Description

A hybrid rocket system optimizes performance by starting the rocket engines at higher altitudes, where air density is low, instead of launching it from the ground. The system uses propellers for the initial ascent to the desired altitude. This enhances fuel efficiency, reduces environmental impact, and optimizes ascent trajectories for sustainable and versatile functions.