DocumentCode
3237377
Title
Designing electronic systems for space
Author
Sunderland, David A. ; Lerma, Jaime ; McKay, Anthony L.
Author_Institution
Boeing Space & Intell. Syst., El Segundo, CA
fYear
2008
fDate
13-15 Oct. 2008
Firstpage
171
Lastpage
177
Abstract
This tutorial presents the unique issues that must be considered when designing electronics for space applications (including, but not limited to, radiation effects), and how key satellite system building blocks are affected by these issues. We review the common design techniques used to mitigate these effects, with an emphasis on those used within custom bipolar integrated circuits. Finally, we discuss the requirements for characterization and qualification of the resulting products.
Keywords
bipolar integrated circuits; space vehicle electronics; custom bipolar integrated circuits; electronic systems; satellite system; space applications; space vehicle electronics; spacecraft; Aerospace electronics; Artificial satellites; Bipolar integrated circuits; Ionizing radiation; Job shop scheduling; Land surface temperature; Radiation effects; Single event upset; Solar heating; Space vehicles; bipolar integrated circuits; radiation effects; radiation hardening; reliability; space vehicle electronics;
fLanguage
English
Publisher
ieee
Conference_Titel
Bipolar/BiCMOS Circuits and Technology Meeting, 2008. BCTM 2008. IEEE
Conference_Location
Monteray, CA
ISSN
1088-9299
Print_ISBN
978-1-4244-2725-3
Electronic_ISBN
1088-9299
Type
conf
DOI
10.1109/BIPOL.2008.4662737
Filename
4662737
Link To Document