准静态载荷空间鉴定试验

2021 IEEE 8th International Workshop on Metrology for AeroSpace (MetroAeroSpace) Pub Date : 2021-06-23 DOI:10.1109/MetroAeroSpace51421.2021.9511773

M. Orefice, V. Quaranta, G. Bruno, Giuseppe Martinotti, Carmine Carandente Tartaglia

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引用次数: 0

摘要

卫星的设计和测试能够承受发射和上升阶段的静态和动态运行载荷。卫星结构设计的验证通常通过试验和(或)分析进行。本文介绍了静载试验方法，重点介绍了正弦爆破准静载试验。为了克服与正弦脉冲测试相关的主要问题，本文将介绍一个测试程序。最后将讨论在6U立方体卫星上进行的测试结果。

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Quasi-static load space qualification test

Satellites are designed and tested to withstand to static and dynamic operative loads during the launch and the ascent phase. The validation of the structural design of the satellite is generally performed by tests and/or analysis. The paper presents the static load test methods with a focus on the sine-burst quasi-static load test. A test procedure will be presented in order to overcome the main issues related to a sine-burst test. Finally test results performed on a 6U Cubesat will be discussed.

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来源期刊

2021 IEEE 8th International Workshop on Metrology for AeroSpace (MetroAeroSpace)

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