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.
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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 |
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代理人 |
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主权项 |
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地址 |
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