금속 프린팅을 활용한 초소형위성 구조체 설계 및 해석Structural Analysis and Design of Nanosatellite with 3D Printed Aluminum Frame
- Other Titles
- Structural Analysis and Design of Nanosatellite with 3D Printed Aluminum Frame
- Authors
- 이용호; 이민태; 권상은; 김경희; 박재현
- Issue Date
- Feb-2023
- Publisher
- 한국기계가공학회
- Keywords
- CubeSat( ); Structure Analysis( ); Stress( ); Deformation( ); Metal 3D Printing 큐브셋 구조해석 응력 변형( 3D )
- Citation
- 한국기계가공학회지, v.22, no.2, pp 33 - 38
- Pages
- 6
- Indexed
- KCI
- Journal Title
- 한국기계가공학회지
- Volume
- 22
- Number
- 2
- Start Page
- 33
- End Page
- 38
- URI
- https://scholarworks.gnu.ac.kr/handle/sw.gnu/30258
- DOI
- 10.14775/ksmpe.2022.22.02.033
- ISSN
- 1598-6721
2288-0771
- Abstract
- Recently, 3D printing has been steadily growing in related technologies and markets because it has the advantage ofmaking lighter and more complex products. Moreover, 3D printing of metallic materials has been commercializedwith increasing number of applications in aerospace. This study presents the design of a 2U nanosatellite having analuminum 3D printed structure and its structural analysis results at the launch environment. The volume and weightof the target model followed CubeSat's 2U standard, and the material used was AlSi10Mg. Based on this, static loadanalysis and modal analysis were performed on the structure using finite element analysis according to the launchenvironment standards required by GSFC-STD-7000. As a result of the analysis, it was confirmed that the 3D-printedframe is structurally safe in all cases, and it could sufficiently replace the general structural frame similar to theAl6000 and Al7000 series materials produced by the machining process.
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