Design optimisation and comparison of propulsion systems for sounding rockets☆
Sounding rockets serve as vital platforms for conducting scientific experiments in the upper atmosphere and near-space environments. These suborbital vehicles are widely used for atmospheric research, microgravity experiments, and testing space technologies. A critical component in their development is the optimisation and selection of appropriate propulsion systems. This blog delves into the design strategies and comparative analysis of propulsion systems for sounding rockets. 🔧 What Is Propulsion System Design Optimisation? Design optimisation involves adjusting variables such as thrust-to-weight ratio, burn time, nozzle efficiency, and mass flow rate to achieve peak performance. For sounding rockets, this optimisation is essential to ensure cost-effectiveness, reliable altitude achievement, and minimal payload disturbance. Engineers utilise computational simulations, trajectory models, and thermal analysis tools to fine-tune propulsion parameters. ⚙️ Types of Propulsion S...