DocumentCode
1640731
Title
EMC qualification of the ATV spacecraft
Author
Schaffar, A. ; Ramos, M. ; Laget, Ph
Author_Institution
EADS Astrium Space Transp., Les Mureaux, France
fYear
2010
Firstpage
1
Lastpage
2
Abstract
This paper focuses on the Automated Transfer Vehicle qualification process mainly based on tests at various performed at levels. It presents the system EMC specifications, the development logic, the test process and results, and the conclusions. The ATV is an European Space Agency Program with ASTRIUM Space Transportation as Prime Contractor. Its mission is to provide the International Space Station with re-boost and attitude control functions, and deliver water, gas, propellant and dry cargo.
Keywords
aircraft testing; electromagnetic compatibility; space vehicles; ATV spacecraft; EMC qualification; EMC specification; attitude control function; automated transfer vehicle qualification; Aerospace electronics; Electromagnetic compatibility; Electrostatic discharge; HDTV; Qualifications; Resistance heating; Safety;
fLanguage
English
Publisher
ieee
Conference_Titel
Antenna Technology and Applied Electromagnetics & the American Electromagnetics Conference (ANTEM-AMEREM), 2010 14th International Symposium on
Conference_Location
Ottawa, ON
Print_ISBN
978-1-4244-5049-7
Electronic_ISBN
978-1-4244-5050-3
Type
conf
DOI
10.1109/ANTEM.2010.5552513
Filename
5552513
Link To Document