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The Design and Implementation of NASA's Advanced Flight Computing Module

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dc.contributor.author Alkakaj, Leon en_US
dc.contributor.author Straedy, Richard en_US
dc.contributor.author Jarvis, Bruce en_US
dc.date.accessioned 2004-10-05T06:20:11Z
dc.date.available 2004-10-05T06:20:11Z
dc.date.issued 1995-03-15 en_US
dc.identifier.clearanceno 94-1363 en_US
dc.identifier.uri http://hdl.handle.net/2014/33518
dc.description.abstract This paper describes a working flight computer Multichip Module developed jointly by JPL and TRW under their respective research programs in a collaborative fashion. The MCM is fabricated by nCHIP and is packaged within a 2 by 4 inch Al package from Coors. This flight computer module is one of three modules under development by NASA's Advanced Flight Computer (AFC) program. Further development of the Mass Memory and the programmable I/O MCM modules will follow. The three building block modules will then be stacked into a 3D MCM configuration. The mass and volume of the flight computer MCM achieved at 89 grams and 1.5 cubic inches respectively, represent a major enabling technology for future deep space as well as commercial remote sensing applications. en_US
dc.format.extent 462136 bytes
dc.format.mimetype application/pdf
dc.language.iso en_US
dc.subject.other computer design space applications multichip modules cost reduction packaging flight computer MCM en_US
dc.title The Design and Implementation of NASA's Advanced Flight Computing Module en_US


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