2011
DOI: 10.1134/s1990793111060169
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Combustion of zirconium-containing model compositions of solid propellant

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Cited by 4 publications
(2 citation statements)
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“…In companion experimental activities [4], solid propellant formulations containing up to 40% Zr were found to burn stable over a range of pressure from 20 to 80 atm. Using Zr, it was possible to obtain burning rates and burning rate exponents close to the values typical of compositions based on Al.…”
Section: Progress In Propulsion Physicsmentioning
confidence: 99%
“…In companion experimental activities [4], solid propellant formulations containing up to 40% Zr were found to burn stable over a range of pressure from 20 to 80 atm. Using Zr, it was possible to obtain burning rates and burning rate exponents close to the values typical of compositions based on Al.…”
Section: Progress In Propulsion Physicsmentioning
confidence: 99%
“…Metal Zr has the advantages of high volumetric heat of combustion heat (77.77 kJ/cm 3 ), moderate ignition temperature (200~400 °C) and good burning stability. These advantages make Zr powder an important component in energetic materials such as propellants and pyrotechnics [1][2][3][4][5] . Previous studies demonstrated that ignition and combustion properties of pure Zr and Zr-containing energetic compositions could be significantly influenced by particle sizes or types of Zr.…”
mentioning
confidence: 99%