About this document
Solid Propellant Combustion Analysis by dhruvchaturvediiitb is a document available to read on EtoBox.
The document discusses the ballistic properties of solid propellants, focusing on burn rate, temperature sensitivity, and mass balance equations. It outlines different burning behaviors characterized by pressure indices and presents various measurement techniques for burn rates, including Crawford bomb and Acoustic Emission Technique. Additionally, it mentions the stability of solid rocket motors and provides references for further lectures on solid rocket performance and design.
- Author
- dhruvchaturvediiitb
- Language
- EN