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T-Burner tests of an Al/HTPB propellant in conjunction with a Pulsed DB/AB Method were conducted to find an acoustic amplification factor. Aluminum-fr ee and aluminum-heavy propellants were examined. Instant surface ignition was successfully made by the use of a supplementary propellant of fractionally higher reaction rate. With the prese nce of higher aluminum concentration in the propellants, the pressure perturbations were promptly dampe d down and the pressure fluctuations were no longer dispersive. Addition of aluminum particles into the propellant was advantageous for stabilizing pressure-coupled unstable waves.   ,    HTPB/AP     , Pulsed DB/AB T-burner  .     ,          .     T-burner         ,          .     ,     .Key Words: Solid Propellant(), Combustion Response(), T-burner(T-), Fast Ignition Disk(), Pulsed DB/AB Method( DB/AB )Received 2 December 2013 / Revised 1 March 2014 / Accepted 8 Ma rch 2014

han'gug cujin gonghag hoeji/han-guk chujin-gong hakoeji

Measurement of Pressure-coupled Combustion Instability Characteristics : Acoustic Attenuation by Particulate Matter(Al) and Combustion Response of Solid Propellant