The rocket interferometer tracking (RIT) system

Descripción del Articulo

A Rocket Interferometer Tracking (RIT) system is described. It uses a modified 108 Me Minitrack receiver converted for 73.6 Me operation and a newly developed phase measuring system. The output of the system is real time direction cosine data for two channels, East-West and North-South, in analog an...

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Detalles Bibliográficos
Autores: Spafford, Michael, Wiack, Richard, Woodman Pollitt, Ronald Francisco
Formato: objeto de conferencia
Fecha de Publicación:1965
Institución:Instituto Geofísico del Perú
Repositorio:IGP-Institucional
Lenguaje:inglés
OAI Identifier:oai:repositorio.igp.gob.pe:20.500.12816/552
Enlace del recurso:http://hdl.handle.net/20.500.12816/552
Nivel de acceso:acceso abierto
Materia:Artificial satellites
Rockets
Interferometry
Antennas
http://purl.org/pe-repo/ocde/ford#1.05.01
Descripción
Sumario:A Rocket Interferometer Tracking (RIT) system is described. It uses a modified 108 Me Minitrack receiver converted for 73.6 Me operation and a newly developed phase measuring system. The output of the system is real time direction cosine data for two channels, East-West and North-South, in analog and digital form. The analog data are recorded on an x-y recorder and on a strip chart recorder; and the digital data are automatically recorded on punched tape. The RIT system has been integrated with the ranging portion of the Radio Doppler Interferometer Tracking system (RADINT) at the Wallops Island Launch facility, and records the range data on the same punched tape.
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