Show simple item record

dc.contributor.authorBennett, Toby
dc.contributor.authorLooney, Kristin
dc.contributor.authorChesney, Jim
dc.date.accessioned2016-06-14T18:43:57Z
dc.date.available2016-06-14T18:43:57Z
dc.date.issued1991-11
dc.identifier.issn0884-5123
dc.identifier.issn0074-9079
dc.identifier.urihttp://hdl.handle.net/10150/613098
dc.descriptionInternational Telemetering Conference Proceedings / November 04-07, 1991 / Riviera Hotel and Convention Center, Las Vegas, Nevadaen_US
dc.description.abstractSpace telemetry data processing elements for flight and ground systems are currently developed using discrete components on a project-by-project basis. The adoption of various standards, such as those recommended by the Consultative Committee for Space Data Systems (CCSDS), brings commonality of requirements across future NASA communications elements and affords the opportunity to create standard components to meet these requirements. Over the past five years, NASA’s Goddard Space Flight Center (GSFC) has developed a series of high performance Very Large Scale Integration (VLSI) components for space data systems. These standard components have enabled the development of high performance data systems that are an order of magnitude more compact and cost effective than systems of the previous generation. Recent advances in design automation tools and integrated circuit densities have yielded the means to achieve yet another leap in the integration levels, performance and cost reduction of space data systems. Design automation tools can generate complex integrated circuit designs from high level technology independent functional descriptions. A single reusable functional description can be targeted to a variety of circuit technologies including CMOS, ECL and GaAs. With available densities of over 1 million integrated transistors in both CMOS and GaAs technologies, standard components integrating multiple processing elements are realizable for both flight and ground projects. This paper describes the ongoing efforts of the Microelectronics Systems Branch at GSFC to create highly integrated components to meet functions outlined by the CCSDS using design automation techniques.
dc.description.sponsorshipInternational Foundation for Telemeteringen
dc.language.isoen_USen
dc.publisherInternational Foundation for Telemeteringen
dc.relation.urlhttp://www.telemetry.org/en
dc.rightsCopyright © International Foundation for Telemeteringen
dc.titleNEXT GENERATION FUNCTIONAL COMPONENTS FOR SPACE TELEMETRY DATA PROCESSINGen_US
dc.typetexten
dc.typeProceedingsen
dc.contributor.departmentNASA, Goddard Space Flight Centeren
dc.identifier.journalInternational Telemetering Conference Proceedingsen
dc.description.collectioninformationProceedings from the International Telemetering Conference are made available by the International Foundation for Telemetering and the University of Arizona Libraries. Visit http://www.telemetry.org/index.php/contact-us if you have questions about items in this collection.en
refterms.dateFOA2018-06-14T00:06:05Z
html.description.abstractSpace telemetry data processing elements for flight and ground systems are currently developed using discrete components on a project-by-project basis. The adoption of various standards, such as those recommended by the Consultative Committee for Space Data Systems (CCSDS), brings commonality of requirements across future NASA communications elements and affords the opportunity to create standard components to meet these requirements. Over the past five years, NASA’s Goddard Space Flight Center (GSFC) has developed a series of high performance Very Large Scale Integration (VLSI) components for space data systems. These standard components have enabled the development of high performance data systems that are an order of magnitude more compact and cost effective than systems of the previous generation. Recent advances in design automation tools and integrated circuit densities have yielded the means to achieve yet another leap in the integration levels, performance and cost reduction of space data systems. Design automation tools can generate complex integrated circuit designs from high level technology independent functional descriptions. A single reusable functional description can be targeted to a variety of circuit technologies including CMOS, ECL and GaAs. With available densities of over 1 million integrated transistors in both CMOS and GaAs technologies, standard components integrating multiple processing elements are realizable for both flight and ground projects. This paper describes the ongoing efforts of the Microelectronics Systems Branch at GSFC to create highly integrated components to meet functions outlined by the CCSDS using design automation techniques.


Files in this item

Thumbnail
Name:
ITC_1991_91-814.pdf
Size:
337.9Kb
Format:
PDF

This item appears in the following Collection(s)

Show simple item record