About this document
Thrust Correlation in Solid Rocket Motors by Mohamed ElFarran is a document available to read on EtoBox.
The article discusses the correlation between the thrust of solid propellant rocket motors (SPRMs) and the initial temperature of the propellant charge, emphasizing the significant impact of initial combustion temperature on propulsion characteristics. It highlights the necessity of controlling the nozzle geometry to maintain constant thrust and chamber pressure, with experimental results demonstrating a consistent thrust force across varying initial temperatures. The study concludes that theoretical models
- Author
- Mohamed ElFarran
- Language
- EN