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dc.contributor.authorCosme, Rafael
dc.contributor.authorLokerson, Donald
dc.date.accessioned2016-05-14T00:27:36Zen
dc.date.available2016-05-14T00:27:36Zen
dc.date.issued1975-10en
dc.identifier.issn0884-5123en
dc.identifier.issn0074-9079en
dc.identifier.urihttp://hdl.handle.net/10150/609349en
dc.descriptionInternational Telemetering Conference Proceedings / October 14-16, 1975 / Sheraton Inn, Silver Spring, Marylanden_US
dc.description.abstractA low power, small size, building block type of central data system has been designed for use in a number of explorer type missions. The Data Multiplexing Unit was designed to satisfy a wide range of requirements among the several spacecraft. The resulting design includes preprogrammed Read Only Memories (ROM's) to generate the telemetry format tailored to the particular mission requirements. The relatively small size and low weight and power dissipation attained was largely due to the use of PMOS technology. The addition of sub-commutators in groups adequate to meet the particular spacecraft requirements allows low data rate experiments to be time multiplexed into a single main input channel for a more efficient data collection and processing operation.
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.titleMultimission Spacecraft Dataplexeren_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.dateFOA2018-09-11T10:25:30Z
html.description.abstractA low power, small size, building block type of central data system has been designed for use in a number of explorer type missions. The Data Multiplexing Unit was designed to satisfy a wide range of requirements among the several spacecraft. The resulting design includes preprogrammed Read Only Memories (ROM's) to generate the telemetry format tailored to the particular mission requirements. The relatively small size and low weight and power dissipation attained was largely due to the use of PMOS technology. The addition of sub-commutators in groups adequate to meet the particular spacecraft requirements allows low data rate experiments to be time multiplexed into a single main input channel for a more efficient data collection and processing operation.


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