| 飞行器防空间静电放电设计和试验技术 |
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| 引用本文： | 曹敏.飞行器防空间静电放电设计和试验技术[J].装备环境工程,2011,8(4):117-121. |
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| 作者姓名： | 曹敏 |
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| 作者单位： | 上海卫星工程研究所,上海,200240 |
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| 摘 要： | 结合某飞行器的特点,以及产品在轨飞行期间遭遇的空间静电放电(SESD)环境,研究了在没有可借鉴的条件下,如何通过分析提出大型天线及本体的空间静电放电防护设计目标,根据产品实际情况设计了分段实施的措施,运用等效理念设计了试验子样和测试方案,策划了设计元器件、原材料、天线系统、飞行器等不同层面的试验验证技术和方法.
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| 关 键 词： | 飞行器 空间静电充放电 辐射干扰 传导干扰 设计 验证 |
| 收稿时间： | 2011/1/18 0:00:00 |
| 修稿时间： | 2011/8/15 0:00:00 |
SESD-proof Design and Test Technique of Spacecraft |
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| CAO Min.SESD-proof Design and Test Technique of Spacecraft[J].Equipment Environmental Engineering,2011,8(4):117-121. |
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| Authors: | CAO Min |
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| Institution: | CAO Min(Shanghai Institute of Satellite Engineering,Shanghai 200240,China) |
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| Abstract: | The characteristics of a spacecraft and the space electrostatic discharge environment encountered by the spacecraft during on-orbit flight process were introduced.The way to determined space electrostatic discharge(SESD) protection objective of large antenna and antenna body was put forward under the condition of no reference.A segmented execution method was designed based on the characteristics of the product.specimen and test scheme were designed with equivalent concept.Experiment validation techniques an... |
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| Keywords: | spacecraft space electrostatic discharge radiated interference conducted interference design validation |
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