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What is Hybrid Rocket Fuel Burning Rate Analysis about?

This document summarizes the solution to a practice problem analyzing the effects of mass flux and normal acceleration on the burning rate of a hybrid rocket fuel. It presents equations to model the burning rate as dependent on mass flux and normal acceleration. The burning rate is solved through iteration. At a normal acceleration of 500g, the calculated burning rate is 0.0173 m/s, which is 2.46 times the base burning rate of 0.00703 m/s due only to mass flux. A graph shows the regression rates versus norm

Author

Harpreet Singh Sahota

Language

EN