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>Structural, Thermal Optical Modeling of CUBESAT GEO Based Orbit Camera Payload 14th annual Advanced Maui Optical and Space Surveillance Technologies (AMOS) Conference, September 10-13,2013, Maui, Hawaii Manuscript Number 1203299
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Structural, Thermal Optical Modeling of CUBESAT GEO Based Orbit Camera Payload 14th annual Advanced Maui Optical and Space Surveillance Technologies (AMOS) Conference, September 10-13,2013, Maui, Hawaii Manuscript Number 1203299
This paper presents the results of a team of students at California State Polytechnic University at Pomona (Cal Poly Pomona) who have been working on a multi-disciplinary team capstone senior project sponsored by Caltech's NASA Jet Propulsion Laboratory (JPL). Results obtained from Structural, Thermal Optical (STOP) Modeling of a CUBESAT GEO based orbit instrumentation payload using SIEMENS PLM NX Space Systems Thermal and NX NASTRAN Finite Element Analysis (FEA) tool suite is the focus of this paper. Results from environmental loading used to predict the thermal performance of a 4U-CUBESAT instrument payload composed of and IR camera surveillance based sub-system are presented. These thermal predictions are used to perform top-level STOP analysis in order to form an optical Figure of Merit (FOM) parameter for performance characterization.
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机译:本文介绍了加利福尼亚州立工业大学的一组学生团队(Cal Poly Pomona)的成果,他们一直在努力由Caltech NASA Jet推进实验室(JPL)赞助的多学科团队Capstone高级项目。使用西门子PLM NX Space Systems的CubeSat Geo基于轨道仪表有效载荷的结构,热光学(STOP)建模获得的结果热量和NX Nastran有限元分析(FEA)工具套件是本文的重点。介绍了用于预测由IR相机监控基于子系统组成的4U立方体仪器有效载荷的环境载荷的结果。这些热预测用于执行顶级停止分析,以便形成用于性能表征的Merit(FOM)参数的光学图。
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