X-33 INTEGRATED TEST FACILITY EXTENDED RANGE SIMULATION
dc.contributor.author | Sharma, Ashley | |
dc.date.accessioned | 2016-05-18T21:31:36Z | |
dc.date.available | 2016-05-18T21:31:36Z | |
dc.date.issued | 1998-10 | |
dc.identifier.issn | 0884-5123 | |
dc.identifier.issn | 0074-9079 | |
dc.identifier.uri | http://hdl.handle.net/10150/609695 | |
dc.description | International Telemetering Conference Proceedings / October 26-29, 1998 / Town & Country Resort Hotel and Convention Center, San Diego, California | en_US |
dc.description.abstract | In support of the X-33 single-stage-to-orbit program, NASA Dryden Flight Research Center was selected to provide continuous range communications of the X-33 vehicle from launch at Edwards Air Force Base, California, through landing at Malmstrom Air Force Base, Montana, or at Michael Army Air Field, Utah. An extensive real-time range simulation capability is being developed to ensure successful communications with the autonomous X-33 vehicle. This paper provides an overview of the various levels of simulation, integration, and test being developed to support the X-33 extended range subsystems. These subsystems include the flight termination system, L-band command uplink subsystem, and S-band telemetry downlink subsystem. | |
dc.description.sponsorship | International Foundation for Telemetering | en |
dc.language.iso | en_US | en |
dc.publisher | International Foundation for Telemetering | en |
dc.relation.url | http://www.telemetry.org/ | en |
dc.rights | Copyright © International Foundation for Telemetering | en |
dc.subject | X-33 Experimental Aircraft | en |
dc.subject | Integration and Test Facility | en |
dc.subject | Range Simulation | en |
dc.subject | Dynamic Ground Station Analysis | en |
dc.subject | Plasma Attenuation | en |
dc.subject | Link Margin | en |
dc.title | X-33 INTEGRATED TEST FACILITY EXTENDED RANGE SIMULATION | en_US |
dc.type | text | en |
dc.type | Proceedings | en |
dc.contributor.department | National Aeronautics and Space Administration | en |
dc.identifier.journal | International Telemetering Conference Proceedings | en |
dc.description.collectioninformation | Proceedings 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.dateFOA | 2018-06-22T21:56:01Z | |
html.description.abstract | In support of the X-33 single-stage-to-orbit program, NASA Dryden Flight Research Center was selected to provide continuous range communications of the X-33 vehicle from launch at Edwards Air Force Base, California, through landing at Malmstrom Air Force Base, Montana, or at Michael Army Air Field, Utah. An extensive real-time range simulation capability is being developed to ensure successful communications with the autonomous X-33 vehicle. This paper provides an overview of the various levels of simulation, integration, and test being developed to support the X-33 extended range subsystems. These subsystems include the flight termination system, L-band command uplink subsystem, and S-band telemetry downlink subsystem. |