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dc.contributor.authorHilliard, Lawrence M.*
dc.date.accessioned2016-06-29T19:06:07Z
dc.date.available2016-06-29T19:06:07Z
dc.date.issued1988-10
dc.identifier.issn0884-5123
dc.identifier.issn0074-9079
dc.identifier.urihttp://hdl.handle.net/10150/615064
dc.descriptionInternational Telemetering Conference Proceedings / October 17-20, 1988 / Riviera Hotel, Las Vegas, Nevadaen_US
dc.description.abstractShaped omni and modular array antenna concepts are being baselined for use on operations with the NASA Space Network and the High Resolution Solar Observatory (HRSO) Satellite Free Flyer Concept. This mission requires 16 MBPS return links, 1 KBPS multiple access links, and a completely redundant set of gimballed antennas to support these links with 90% continuous coverage from TDRSS (Tracking and Data Relay Satellite System). This presentation will discuss in detail how the flexibility of these components enabled mission planners to tradeoff spacecraft options without sacrificing mission objectives.
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.titleNASA-GSFC Research Developments Evolve into HRSO Satellite Conceptsen_US
dc.typetexten
dc.typeProceedingsen
dc.contributor.departmentNASA-GSFCen
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.dateFOA2018-09-11T14:05:06Z
html.description.abstractShaped omni and modular array antenna concepts are being baselined for use on operations with the NASA Space Network and the High Resolution Solar Observatory (HRSO) Satellite Free Flyer Concept. This mission requires 16 MBPS return links, 1 KBPS multiple access links, and a completely redundant set of gimballed antennas to support these links with 90% continuous coverage from TDRSS (Tracking and Data Relay Satellite System). This presentation will discuss in detail how the flexibility of these components enabled mission planners to tradeoff spacecraft options without sacrificing mission objectives.


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