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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。
Considering the characteristics of an aircraft and the space electrostatic discharge (SESD) environment encountered during the orbital flight of the aircraft, this paper studies how to design the space electrostatic discharge protection design goals for large antennas and ontology under the condition of no reference, The actual situation has been designed to implement the measures in stages. The equivalent sub-concept has been used to design the test sub-sample and the test plan. The experimental verification techniques and methods for designing components, raw materials, antenna systems and aircraft have been planned.