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 :
بازگشت