Numerical Analysis Approach to Aid in Launch Vehicle Lightning Effects Protection Design

被引:0
作者
Kitaygorsky, Jennifer [1 ]
机构
[1] Electro Magnet Applicat, Lakewood, CO 80228 USA
来源
2020 IEEE INTERNATIONAL SYMPOSIUM ON ELECTROMAGNETIC COMPATIBILITY AND SIGNAL & POWER INTEGRITY VIRTUAL SYMPOSIUM(IEEE EMC+SIPI) | 2020年
关键词
lightning; rocket; indirect effects; ATL; launch vehicle; transients; FDTD;
D O I
暂无
中图分类号
TM [电工技术]; TN [电子技术、通信技术];
学科分类号
0808 ; 0809 ;
摘要
Lightning is a critical safety issue for all aerospace vehicles. Commercial aircraft are protected from the effects of lightning strikes per the FAA regulation. Some launch vehicles rely on lightning launch criteria rules to avoid lightning. That launch vehicles can and do get struck by lightning has been recently demonstrated by the Soyuz rocket during a satellite launch on May 27, 2019, through which the rocket persevered and went on to complete its mission successfully (it is unclear what kind of lightning protection design was implemented). In this work we discuss how numerical analysis provides an in-depth understanding of the effects of a lightning strike on a launch vehicle by simulating lightning coupling processes and obtaining transient levels throughout the vehicle on bonds, harnesses, and at box interfaces. This understanding aids in the vehicle lightning protection design and reduces elements of an expensive test program. We accomplish this through a simulation example of a notional launch vehicle.
引用
收藏
页码:328 / 333
页数:6
相关论文
共 10 条
  • [1] [Anonymous], 2013, 5412B ARP
  • [2] [Anonymous], MILSTS461
  • [3] [Anonymous], 2011, 20136B AC
  • [4] Gabriasak M., 2019, HDB AEROSPACE ELECTR
  • [5] Godfrey R., 1970, NASA TECHNICAL NOTE
  • [6] Kostogorova-Beller Y, 2017, INT C LIGHTNING STAT
  • [7] Lalonde D., 2015, INT C LIGHTN STAT EL
  • [8] O'Connor B., 2007, LEAD VITS M MARCH 5
  • [9] Weber C., 2019, INT C LIGHTN STAT EL
  • [10] Weber C., 2015, PROC INT C LIGHTNING