DocumentCode :
1602093
Title :
EMI/EMC, lightning, radiation shielding verification approach for the Dragon COTS spacecraft: Part II
Author :
Elkman, W. ; Trinh, J. ; McCaughey, P. ; Chen, W.
Author_Institution :
Space Exploration Technol., Hawthorne, CA, USA
fYear :
2011
Firstpage :
647
Lastpage :
652
Abstract :
Designing the Dragon COTS (Commercial Orbital Transfer System) for EMI/EMC interface compliance to the International Space Station (ISS) is a complex task. It involves designing Dragon for self-compatibility, compatibility with the Falcon 9 Launch Vehicle, designing to the LEO Space radiation environment, and designing for interface compatibility to the ISS mechanical, electrical and RF interfaces. This paper, Part II, describes the Space Exploration Technologies analysis and test verification methods used to achieve Dragon spacecraft self-compatibility, compatibility with the Eastern Launch Range RF requirements, and interface compatibility to the ISS requirements for EMC emissions and susceptibility.
Keywords :
electromagnetic compatibility; electromagnetic interference; lightning protection; space vehicle electronics; Dragon COTS spacecraft; EMI/EMC interface compliance; Space Exploration Technologies analysis; commercial orbital transfer system; interface compatibility; international space station; lightning; radiation shielding verification; self compatibility; test verification methods; Aerospace electronics; Lightning; Radar imaging; Radio frequency; Surge protection; Surges;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Electromagnetic Compatibility (EMC), 2011 IEEE International Symposium on
Conference_Location :
Long Beach, CA, USA
ISSN :
2158-110X
Print_ISBN :
978-1-4577-0812-1
Type :
conf
DOI :
10.1109/ISEMC.2011.6038390
Filename :
6038390
Link To Document :
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