JPL Technical Report Server

The Design of a Fault-Tolerant COTS-Based Bus Architecture For Space Applications

Show simple item record

dc.contributor.author Chau, S. en_US
dc.contributor.author Alkalai, L. en_US
dc.contributor.author Tai, A. en_US
dc.date.accessioned 2004-09-23T22:47:40Z
dc.date.available 2004-09-23T22:47:40Z
dc.date.issued 1999-06-15 en_US
dc.identifier.citation 29th International Symposium on Fault-Tolerance Computing en_US
dc.identifier.citation Madison, Wisconsin, USA en_US
dc.identifier.clearanceno 99-0044 en_US
dc.identifier.uri http://hdl.handle.net/2014/16654
dc.description.abstract The high-performance, scalability and miniaturization requirements together with the power, mass and cost constraints mandate the use of commercial-off-the-shelf (COTS) components and standards in the X2000 avionics system architecture for deep-space missions. en_US
dc.format.extent 1386324 bytes
dc.format.mimetype application/pdf
dc.language.iso en_US
dc.subject.other commercial data bus space applications en_US
dc.title The Design of a Fault-Tolerant COTS-Based Bus Architecture For Space Applications en_US


Files in this item

This item appears in the following Collection(s)

Show simple item record

Search


Browse

My Account