Browsing by Subject "AP"
Now showing items 1-3 of 3
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(2017-05-02)Composite solid propellants are typically used in rocket propulsion systems due to their simplicity and relatively low cost. They are mixtures of the fuel, oxidizer, and various catalysts. Oftentimes, bonding agents and ...
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(2017-04-27)The burning rates of IPDI-cured AP/HTPB propellants with a standard curing ratio were analyzed. It is well known that the particle size of AP as well as their concentration greatly affects the burning rate, yet there exists ...
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(2013-07-22)Presented in this thesis is the development of a new method to achieve plateau burning profiles in composite solid propellants. Propellants were formulated using ammonium perchlorate (AP) as the oxidizer and hydroxyl ...