Structural design and analysis of test mass module for DECIGO Pathfinder

被引:1
|
作者
Wakabayashi, Y. [1 ]
Obuchi, Y. [2 ]
Okada, N. [2 ]
Torii, Y. [2 ]
Ejiri, Y. [1 ]
Suzuki, R. [1 ]
Ueda, A.
Kawamura, S. [2 ]
Araya, A. [3 ]
Ando, M. [4 ]
Sato, S. [5 ]
Sugamoto, A. [1 ]
机构
[1] Ochanomizu Univ, Dept Phys, Bunkyo Ku, 2-1-1 Ohtsuka, Tokyo 1128610, Japan
[2] Natl Astron Observ Japan, Tokyo 1818588, Japan
[3] Univ Tokyo, Earthquake Res Inst, Bunkyo ku, Tokyo 1130032, Japan
[4] Kyoto Univ, Grad Sch Sci, Div Phys & Astron, Kyoto 6068502, Japan
[5] Hosei Univ, Fac Engn, Tokyo 1848584, Japan
关键词
D O I
10.1088/1742-6596/228/1/012047
中图分类号
P1 [天文学];
学科分类号
0704 ;
摘要
Deci-hertz Interferometer Gravitational-Wave Observatory: DECIGO is a project aimed at future detection of deci-hertz gravitational waves in space. DECIGO Pathfinder: DPF is a precursor mission to test the key technologies with one spacecraft. Our work in this article was to examine the strength of the DPF test mass module to ensure that it is sufficiently robust for launch with a launch vehicle. We designed the test mass module, and examined the structural strength of this model by structural analysis, Quasi-static acceleration analysis and Modal analysis using FEA (Finite Element Analysis). We found that the results of each analysis fulfilled all requirements. We are confident that the DPF test mass module will withstand Quasi-static acceleration or coupling with vibration of launch vehicle during launch, if the design matches the current design. For more detail, further analysis including Response analysis and Thermal analysis are recommended. In addition, it will be necessary to lighten the model in the next step.
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页数:6
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