AffiliationMassachusetts Institute of Technology
MetadataShow full item record
RightsCopyright © International Foundation for Telemetering
Collection InformationProceedings 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.
AbstractThe paper describes the design, use and testing of a spacecraft minicomputer. The minicomputer was designed as a controller for the communications payload of a Communications Satellite with about 100 communications channels. Each of the channels has very flexible control including variable data rate, Doppler offset, and flexible routing.
SponsorsInternational Foundation for Telemetering