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dc.contributor.authorGalleher, G. W.
dc.contributor.authorLocklair, A. J.
dc.date.accessioned2016-06-29T20:47:44Z
dc.date.available2016-06-29T20:47:44Z
dc.date.issued1981-10
dc.identifier.issn0884-5123
dc.identifier.issn0074-9079
dc.identifier.urihttp://hdl.handle.net/10150/615071
dc.descriptionInternational Telemetering Conference Proceedings / October 13-15, 1981 / Bahia Hotel, San Diego, Californiaen_US
dc.description.abstractThis paper describes instrumentation and communications techniques used in the data gathering process for presently on going high performance advanced maneuvering reentry vehicle test flights. Transducers and signal conditioning design considerations including flight test results of vibration and acoustic data (gathered simultaneously by eight FM and one 24,824 sps PCM channel), nose and control surface load cells, control actuation, flow rates, control and aerodynamic pressures, heat shield in-depth thermocouples, nose recession (nuclear and acoustic) are discussed. Also presented are the instrumentation techniques used to verify the integrity of the RF subsystem in addition to a description of the PCM, Data Delay and FM video links.
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.rights.urihttp://rightsstatements.org/vocab/InC/1.0/
dc.titleADVANCED MANEUVERING REENTRY VEHICLE INSTRUMENTATION AND COMMUNICATION TECHNIQUESen_US
dc.typetexten
dc.typeProceedingsen
dc.contributor.departmentMcDonnell Douglas Astronautics Companyen
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.dateFOA2018-06-15T21:55:20Z
html.description.abstractThis paper describes instrumentation and communications techniques used in the data gathering process for presently on going high performance advanced maneuvering reentry vehicle test flights. Transducers and signal conditioning design considerations including flight test results of vibration and acoustic data (gathered simultaneously by eight FM and one 24,824 sps PCM channel), nose and control surface load cells, control actuation, flow rates, control and aerodynamic pressures, heat shield in-depth thermocouples, nose recession (nuclear and acoustic) are discussed. Also presented are the instrumentation techniques used to verify the integrity of the RF subsystem in addition to a description of the PCM, Data Delay and FM video links.


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