Use of L- and S-Bond Transmitters for Outer Space Applications
dc.contributor.author | Updike, P. A. | |
dc.date.accessioned | 2016-04-22T17:12:00Z | en |
dc.date.available | 2016-04-22T17:12:00Z | en |
dc.date.issued | 1969-09 | en |
dc.identifier.issn | 0884-5123 | en |
dc.identifier.issn | 0074-9079 | en |
dc.identifier.uri | http://hdl.handle.net/10150/606678 | en |
dc.description | International Telemetering Conference Proceedings / September 15-17, 1969 / Sheraton Park Hotel, Washington, D.C. | en_US |
dc.description.abstract | This paper discusses six engineering problems associated with high reliability L- and S-band transmitters for use in space programs. The problems are: 1. Stable power in thermal vacuum 2. Low intermodulation products 3. Frequency stability 4. Isolation of power and modulation inputs 5. Efficiency 6. Size and weight. It is concluded that further improvements of primary transmitter characteristics, such as size, weight, frequency stability and efficiency will be determined by the rate of progress achieved by the electronic component manufacturers. | |
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.rights.uri | http://rightsstatements.org/vocab/InC/1.0/ | |
dc.title | Use of L- and S-Bond Transmitters for Outer Space Applications | en_US |
dc.type | text | en |
dc.type | Proceedings | en |
dc.contributor.department | Teledyne Telemetry Company | 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 | 2018-04-26T13:43:08Z | |
html.description.abstract | This paper discusses six engineering problems associated with high reliability L- and S-band transmitters for use in space programs. The problems are: 1. Stable power in thermal vacuum 2. Low intermodulation products 3. Frequency stability 4. Isolation of power and modulation inputs 5. Efficiency 6. Size and weight. It is concluded that further improvements of primary transmitter characteristics, such as size, weight, frequency stability and efficiency will be determined by the rate of progress achieved by the electronic component manufacturers. |