发明名称 Propellant composition having a relatively low burn rate exponent and high gas yield
摘要 A method for making a propellant composition that results in a desirable gas output when combusted. The propellant can be part of an inflator used in a vehicle for inflating an air bag. The propellant has a relatively low burn rate exponent of no greater than about 0.7. The propellant is substantially dense, with the propellant having a density that is at least 85% of theoretical density. In making the propellant, its density can be reduced using a roller mill that flattens the propellant to a controlled thickness. The propellant preferably includes phase-stabilized ammonium nitrate and fibrous cellulose.
申请公布号 AU7607400(A) 申请公布日期 2001.04.24
申请号 AU20000076074 申请日期 2000.09.22
申请人 AUTOLIV ASP, INC. 发明人 BRIAN K. HAMILTON
分类号 C06B21/00;C06B31/30;C06D5/06 主分类号 C06B21/00
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