Investigation of the Liquid Breakup Process of Solid Booster Rocket
Abstract
This paper presents a liquid break-up mechanism when aluminum-based fuels are burned in a combustion chamber. The study helps in preventing erosive behavior in a Solid Rocket Motor to improve ballistic performance.
Fields of Study & Subjects
Rocket and propulsion systems research
Energetic Materials and Combustion
Erosion and Abrasive Machining
Publication details
- Journal / source
- AIAA SciTech Forum
- Publication date
- 8 January 2026