Phase measurement/display subsystem for the Apollo re-entry tracking system

Descripción del Articulo

"X-531-63-251, NASA,Goddard Space Flight Center, Maryland, December 13, 1963"
Detalles Bibliográficos
Autor: Woodman Pollitt, Ronald Francisco
Formato: informe técnico
Fecha de Publicación:1963
Institución:Instituto Geofísico del Perú
Repositorio:IGP-Institucional
Lenguaje:inglés
OAI Identifier:oai:repositorio.igp.gob.pe:20.500.12816/528
Enlace del recurso:http://hdl.handle.net/20.500.12816/528
Nivel de acceso:acceso abierto
Materia:Interferometry
Tracking Control Systems
Apollo 1
http://purl.org/pe-repo/ocde/ford#1.05.01
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dc.title.es_ES.fl_str_mv Phase measurement/display subsystem for the Apollo re-entry tracking system
title Phase measurement/display subsystem for the Apollo re-entry tracking system
spellingShingle Phase measurement/display subsystem for the Apollo re-entry tracking system
Woodman Pollitt, Ronald Francisco
Interferometry
Tracking Control Systems
Apollo 1
http://purl.org/pe-repo/ocde/ford#1.05.01
title_short Phase measurement/display subsystem for the Apollo re-entry tracking system
title_full Phase measurement/display subsystem for the Apollo re-entry tracking system
title_fullStr Phase measurement/display subsystem for the Apollo re-entry tracking system
title_full_unstemmed Phase measurement/display subsystem for the Apollo re-entry tracking system
title_sort Phase measurement/display subsystem for the Apollo re-entry tracking system
author Woodman Pollitt, Ronald Francisco
author_facet Woodman Pollitt, Ronald Francisco
author_role author
dc.contributor.author.fl_str_mv Woodman Pollitt, Ronald Francisco
dc.subject.es_ES.fl_str_mv Interferometry
Tracking Control Systems
Apollo 1
topic Interferometry
Tracking Control Systems
Apollo 1
http://purl.org/pe-repo/ocde/ford#1.05.01
dc.subject.ocde.es_ES.fl_str_mv http://purl.org/pe-repo/ocde/ford#1.05.01
description "X-531-63-251, NASA,Goddard Space Flight Center, Maryland, December 13, 1963"
publishDate 1963
dc.date.accessioned.none.fl_str_mv 2016-11-08T03:11:14Z
2017-12-21T19:41:41Z
dc.date.available.none.fl_str_mv 2016-11-08T03:11:14Z
2017-12-21T19:41:41Z
dc.date.issued.fl_str_mv 1963-12-13
dc.type.es_ES.fl_str_mv info:eu-repo/semantics/report
format report
dc.identifier.uri.none.fl_str_mv http://hdl.handle.net/20.500.12816/528
url http://hdl.handle.net/20.500.12816/528
dc.language.iso.es_ES.fl_str_mv eng
language eng
dc.rights.es_ES.fl_str_mv info:eu-repo/semantics/openAccess
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eu_rights_str_mv openAccess
rights_invalid_str_mv https://creativecommons.org/licences/by/4.0/
dc.format.es_ES.fl_str_mv application/pdf
dc.publisher.es_ES.fl_str_mv NASA
dc.source.none.fl_str_mv reponame:IGP-Institucional
instname:Instituto Geofísico del Perú
instacron:IGP
instname_str Instituto Geofísico del Perú
instacron_str IGP
institution IGP
reponame_str IGP-Institucional
collection IGP-Institucional
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spelling Woodman Pollitt, Ronald Francisco2016-11-08T03:11:14Z2017-12-21T19:41:41Z2016-11-08T03:11:14Z2017-12-21T19:41:41Z1963-12-13http://hdl.handle.net/20.500.12816/528"X-531-63-251, NASA,Goddard Space Flight Center, Maryland, December 13, 1963"A combined system consisting of an Interferometer and a Range System has been proposed (Reference #1) for tracking the Apollo spacecraft during the re-entry phase. The system herein discussed processes the output of the above system and performs the following functions.application/pdfengNASAinfo:eu-repo/semantics/openAccesshttps://creativecommons.org/licences/by/4.0/InterferometryTracking Control SystemsApollo 1http://purl.org/pe-repo/ocde/ford#1.05.01Phase measurement/display subsystem for the Apollo re-entry tracking systeminfo:eu-repo/semantics/reportreponame:IGP-Institucionalinstname:Instituto Geofísico del Perúinstacron:IGPORIGINALPhase Measurement_Display Subsystem for the Apolo Re-entry Tracking System-1963.PDFapplication/pdf249425https://repositorio.igp.gob.pe/bitstreams/2f40dc39-09ce-4ed4-8515-342da23b820e/download06a04b7856bcd462cf08922c7bf07fafMD51LICENSElicense.txttext/plain1748https://repositorio.igp.gob.pe/bitstreams/f392d9aa-ecb3-4495-81b7-1bb5f7699ddf/download8a4605be74aa9ea9d79846c1fba20a33MD52THUMBNAILPhase Measurement_Display Subsystem for the Apolo Re-entry Tracking System-1963.PDF.jpgPhase Measurement_Display Subsystem for the Apolo Re-entry Tracking System-1963.PDF.jpgIM Thumbnailimage/jpeg65294https://repositorio.igp.gob.pe/bitstreams/2e21c89c-2945-4541-9319-300b5febb512/download3c137ede091bbe0e4f0516a04cb39783MD53TEXTPhase Measurement_Display Subsystem for the Apolo Re-entry Tracking System-1963.PDF.txtPhase Measurement_Display Subsystem for the Apolo Re-entry Tracking System-1963.PDF.txtExtracted texttext/plain18https://repositorio.igp.gob.pe/bitstreams/3e3eb527-ff6b-40de-9fd8-81671fb3adc2/download1bb607118047afc5c385b82385dd931fMD5420.500.12816/528oai:repositorio.igp.gob.pe:20.500.12816/5282020-12-18 12:03:50.243https://creativecommons.org/licences/by/4.0/info:eu-repo/semantics/openAccessopen.accesshttps://repositorio.igp.gob.peRepositorio Geofísico del Perudspace-help@myu.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Phase measurement/display subsystem for the Apollo re-entry tracking system
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