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This document summarizes a preliminary investigation into using a chemical starting technique for the acid-gasoline rocket propellant system. Specifically, it examines using a small quantity of an igniter fluid that spontaneously ignites with nitric acid to initiate the acid-gasoline combustion reaction. The investigation tested various igniter fluids at temperatures ranging from 500°F to -850°F in a 200-pound thrust engine. It found that ignition was possible down to -850°F with certain aromatic amine and

Author

alex

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EN