维珍轨道发射一号飞行器单事件效应试验验证

2022 IEEE International Symposium on Electromagnetic Compatibility & Signal/Power Integrity (EMCSI) Pub Date : 2022-08-01 DOI:10.1109/EMCSI39492.2022.9889596

W. Elkman, C. Scoby, Umer Qureshi, Andrew Shirali

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引用次数: 0

摘要

本文描述了维珍轨道发射一号(L1)两级LOX/RP-1发射系统的SEE(单事件效应)设计验证方法和质子束验证测试结果，该发射系统能够部署300公斤至500公里太阳同步轨道(SSO)的有效载荷，以及部署500公斤至200公里低地球轨道(LEO)的有效载荷。[9]描述了根据RTCA-DO-160F和MIL-STD-461F定制的EMI/EMC控制程序。[10]报告LauncherOne的电磁兼容性验证过程和结果。

本文章由计算机程序翻译，如有差异，请以英文原文为准。

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Single Event Effects Test Verification for the Virgin Orbit LauncherOne Vehicle

This paper describes the SEE (single event effects) design verification approach and proton beam verification test results for the Virgin Orbit LauncherOne (L1) two stage LOX/RP-1 launch system, capable of deploying payloads up to 300kg to 500km Sun Synchronous Orbit (SSO), and deploying payloads up to 500kg to 200km Low Earth Orbit (LEO). [9] Describes the EMI/EMC Control Program tailored from RTCA-DO-160F and MIL-STD-461F. [10] Reports the Electromagnetic Compatibility (EMC) verification procedures and results for LauncherOne,.

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2022 IEEE International Symposium on Electromagnetic Compatibility & Signal/Power Integrity (EMCSI)

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