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Showing 1 to 1 of 1 for “"Radiative Ignition"”.
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Low flux radiative ignition studies of ammonium perchlorate composite propellants
The vast majority of propellant ignition data has been collected and studied for heat fluxes in the typical, intentional ignition range. However, when a propellant contained within a rocket motor case is exposed to low fluxes in hazardous situations, such as close proximity to a fire, unwanted …