Quasi-Static Structural Test of Satellites

被引:0
|
作者
Yilmaz, Fatih [1 ]
Haktanir, Ozan Oguz [1 ]
Uygur, Ahmet Bilge [1 ]
机构
[1] TAI Turkish Aerosp Ind Inc, Space Syst Assembly Integrat & Test AIT, Ankara, Turkey
关键词
satellite; environmental tests; vibration test system; quasi-static tests;
D O I
暂无
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
Satellites are exposed to simultaneous static and dynamic loads during the launch phase due to launcher acceleration and aerodynamics. Therefore, they are designed and tested to withstand all these loads. From design perspective, a common approach is to combine static and dynamic loads into an equivalent static load which is referred to as quasi-static loads [1]. The validation of the structural design of the satellite is performed by tests and/or analysis. This paper discusses the static load test methods with an emphasis on the acceleration tests performed on vibration test systems.
引用
收藏
页码:421 / 424
页数:4
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