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 US2010294023(A1) 申请公布日期 2010.11.25
申请号 US20090408154 申请日期 2009.03.20
申请人 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
代理机构 代理人
主权项
地址