发明名称 Method of insulating a rocket motor
摘要 Rocket motor insulation compositions are provided. An important component of such insulation compositions is a thermoplastic liquid crystal polymer. Such a polymer provides an ablative insulation which has good performance characteristics during operation of the rocket motor. One such thermoplastic liquid crystal polymer is a wholly aromatic polyester known as VECTRA TM . The insulation may also include fillers such as fibrous fillers and particulate fillers. Typical fibrous fillers include glass or carbon fibers. Typical particulate fillers include materials such as silica, alumina, powdered coal, and the like.
申请公布号 US5352312(A) 申请公布日期 1994.10.04
申请号 US19920927135 申请日期 1992.08.06
申请人 THIOKOL CORPORATION 发明人 GUILLOT, DAVID G.
分类号 B32B37/00;C08K3/00;C08K7/02;F02K9/34;F02K9/97;(IPC1-7):B32B31/20;B65H81/06;C09K21/14;F02K9/08 主分类号 B32B37/00
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