A multi-phase investigation was conducted to quantify the thermal insult produced by the burning of unspent solid rocket propellant in a missile hit scenario. The objectives of this multi-phase investigation were to; identify the thermal conditions produced in the compartment during the missile fuel burning stage, identify the likelihood for ignition of Class A materials in the space and bound the transition time for the ensuring compartment fire. This report summarizes the results of the third and final phase of this investigation.
Propellant Fires in a Simulated Shipboard Compartments: Project HULVUL Phase III
1999
42 pages
Report
Keine Angabe
Englisch
Marine Engineering , Combustion & Ignition , Guided missile warheads , Compartments , Antiship missiles , Shipboard , Fires , Thermal properties , Computerized simulation , Persian gulf , Combustion , Fuels , Ignition , Ship hulls , Detonations , Solid rocket propellants , Propellant fires , Hulvul project , Iscc(Internal ship conflagration control program) , Uss stark , Ffg-31 vessel , Exocet missiles , Hulvul(Hull vulnerability)
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