发明名称 Propellant ignition testing apparatus having a compressively sealable chamber
摘要 A propellant ignition testing apparatus having a compressively sealable chamber. A fixed end plate assembly is fixedly mounted on a support structure. A test chamber assembly having a combustion chamber for accommodating propellant is provided, and an initiator ignites propellant accommodated in the combustion chamber. A moveable end plate is disposed adjacent to the test chamber assembly on a side thereof remote from the fixed end plate assembly. A device is mounted on the support structure for generating a compressive force, with the moveable end plate being operatively connected to a moveable component of the device for moving the moveable end plate toward the test chamber assembly for sandwiching the combustion chamber of the test chamber assembly in a compressively sealed manner between the fixed end plate assembly and the moveable end plate.
申请公布号 US8122757(B2) 申请公布日期 2012.02.28
申请号 US20090408154 申请日期 2009.03.20
申请人 THOMPSON CLAY;KOKSAL HUSEYIN;PIOTROWICZ JESSE;MYERS ALEX;KITTS DANIEL;FLEMING JOSHUA T.;BAKER DAVID M.;MONTANO IAN;NEW MEXICO TECHNICAL RESEARCH FOUNDATION 发明人 THOMPSON CLAY;KOKSAL HUSEYIN;PIOTROWICZ JESSE;MYERS ALEX;KITTS DANIEL;FLEMING JOSHUA T.;BAKER DAVID M.;MONTANO IAN
分类号 G01N33/22 主分类号 G01N33/22
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