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Measuring Missile\'s Suspension Flight Loads Using Built-in Six-component Strain-gage Balance
Author(s): 
Pages: 1403-1409
Year: Issue:  7
Journal: Acta Aeronautica ET Astronautica Sinica

Keyword:  外挂飞行载荷导弹模拟壳体六分量应变天平载荷校准载荷实测;
Abstract: 本文研究了导弹挂飞载荷的飞行实测技术.研制了两套由导弹模拟壳体和内式六分量应变天平组成的测力系统,在进行多项飞行环境适应性、安全性、测试功能性地面试验后,将其左右对称安装在载机截尖三角形翼下,在国内首次对三挂点、大长细比导弹的挂飞载荷进行了飞行实测,试验结果可信可靠.采用与实弹相同的挂装连接方式模拟壳体气动外形和几何尺寸,采用框式双天平一体结构、集中传力、天平校心与测力系统质心重合以及测力系统整体...
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