发明名称 Device for testing behavior of thermal protection element of solid propellant engine of booster rocket or model of booster rocket, has measuring units measuring behavior of thermal protection element and equipped with accelerometer
摘要 <p>The device has measuring units measuring behavior of a thermal protection element and equipped with a ribbon with an optical fiber, an accelerometer, magnetic field measurement units, a deformation gauge, a fluoroscope and Hall effect measurement units. An internal wall of a tubular envelope is covered by two thermal protection elements. An internal diameter of the tubular envelope is provided corresponding to that of a crown. A part of the deformation gauge is located beyond average radius of the crown.</p>
申请公布号 FR2954487(A3) 申请公布日期 2011.06.24
申请号 FR20090006127 申请日期 2009.12.17
申请人 ETAT FRANCAIS 发明人 COLEMARD FRANCOIS
分类号 G01B21/32 主分类号 G01B21/32
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