DocumentCode
2929111
Title
Unique bonding methods for spacecraft
Author
Fos, Joseph E., Jr.
Author_Institution
Lockheed Missiles & Space Co. Inc., Sunnyvale, CA, USA
fYear
1988
fDate
2-4 Aug 1988
Firstpage
412
Lastpage
417
Abstract
Bonding requirements in general are discussed. The additional factors that are introduced for spacecraft bonding are examined and shown to require methods that are outside of normal bonding techniques. An electronic box in a spacecraft is used to illustrate the problems encountered
Keywords
electromagnetic interference; joining processes; space vehicles; EMI aspects; electronic box; spacecraft; unique bonding methods; Aerospace electronics; Bonding; Cable shielding; Connectors; Contacts; Lightning protection; Space heating; Space vehicles; Surface cleaning; Thermal factors;
fLanguage
English
Publisher
ieee
Conference_Titel
Electromagnetic Compatibility, 1988. Symposium Record., IEEE 1988 International Symposium on
Conference_Location
Seattle, WA
Type
conf
DOI
10.1109/ISEMC.1988.14155
Filename
14155
Link To Document