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Evaluation of transient pin-stress requirements for spacecraft launching in Lightning environments: Pain free analysis to alleviate those pin stress headaches
2016
2016 IEEE International Symposium on Electromagnetic Compatibility (EMC)
Spacecraft are generally protected from direct lightning attachment by encapsulation within the payload fairing of a launch vehicle and the ground structures that exist at the launch site. Regardless of where lightning strikes, potentially damaging indirect effects prevail from the coupling of electromagnetic fields into a loop created by outer shield of the payload umbilical. The energy coupled into individual spacecraft circuits is dependent on the umbilical current drive, the cable transfer
doi:10.1109/isemc.2016.7571740
fatcat:qlif43voa5d7vlpprrskizanyq