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dc.contributor.authorStevens, Walter H.
dc.date.accessioned2016-06-24T21:19:24Z
dc.date.available2016-06-24T21:19:24Z
dc.date.issued1989-11
dc.identifier.issn0884-5123
dc.identifier.issn0074-9079
dc.identifier.urihttp://hdl.handle.net/10150/614681
dc.descriptionInternational Telemetering Conference Proceedings / October 30-November 02, 1989 / Town & Country Hotel & Convention Center, San Diego, Californiaen_US
dc.description.abstractThe NASA Marshall Space Flight Center, in Huntsville Alabama, decided in July 1986, to upgrade the development flight instrumentation (DFI) system to monitor the performance of the redesigned solid rocket boosters. On September 29, 1988 Space Shuttle Discovery was successfully launched from Kennedy Space Center, Florida with the redesigned solid rocket boosters carrying the upgraded DFI system which consists of 24 electronic black boxes, over 200 sensors, and 91 cable assemblies. Many contractors supplied parts of the DRI system to NASA Marshall, two thirds of the black boxes were designed and developed by the Aydin Vector Division. The remaining boxes were supplied by Kodak Data Tape, in Pasadena, California and Teledyne Brown Engineering, in Huntsville, Alabama. This paper will show the entire DFI system with particular emphasis on the major subsystems such as the PCM subsystem which consisted of one Programmable Master Encoder and three Remote Slave Encoders, the Frequency Division Multiplexer and the Wideband signal conditioner units. These units conditioned all of the information received from the sensors and multiplexed this data into one encoded PCM data stream and two independent FM composite outputs.
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.titleDevelopment Flight Instrumentation for the Redesigned Solid Rocket Booster for the Space Shuttle Programen_US
dc.typetexten
dc.typeProceedingsen
dc.contributor.departmentAydin Vector Divisionen
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.dateFOA2018-06-20T00:07:56Z
html.description.abstractThe NASA Marshall Space Flight Center, in Huntsville Alabama, decided in July 1986, to upgrade the development flight instrumentation (DFI) system to monitor the performance of the redesigned solid rocket boosters. On September 29, 1988 Space Shuttle Discovery was successfully launched from Kennedy Space Center, Florida with the redesigned solid rocket boosters carrying the upgraded DFI system which consists of 24 electronic black boxes, over 200 sensors, and 91 cable assemblies. Many contractors supplied parts of the DRI system to NASA Marshall, two thirds of the black boxes were designed and developed by the Aydin Vector Division. The remaining boxes were supplied by Kodak Data Tape, in Pasadena, California and Teledyne Brown Engineering, in Huntsville, Alabama. This paper will show the entire DFI system with particular emphasis on the major subsystems such as the PCM subsystem which consisted of one Programmable Master Encoder and three Remote Slave Encoders, the Frequency Division Multiplexer and the Wideband signal conditioner units. These units conditioned all of the information received from the sensors and multiplexed this data into one encoded PCM data stream and two independent FM composite outputs.


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