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A microprocessor based high speed space-borne packet switchThe design and performance evaluation of a single microprocessor based packet switch for use on-board a satellite are presented. The primary design criterion is to maximize the system throughput. A number of protocols and their impact on the switch design are discussed. Stem and processor hardware architectures are described. The flow charts of the software required to accomplish the essential functions are presented and modification needed for use in a multisatellite network are also indicated. Maximum throughput attainable is calculated, desirable characteristics of microprocessors for this application are pointed out. A queue theoretic model of the packet switch has been developed. Analytical relationships of the average waiting times and the queue sizes at the queues and the overall average response time with the various design parameters of the switch have been obtained. A number of graphs showing the effect of variation in the number of input and output lines, data rates, destination functions, speed of output lines and some other design parameters on the performance of the switch are presented and discussed.
Document ID
19800039982
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Arozullah, M.
(Clarkson Coll. of Technology Potsdam, NY, United States)
Crist, S. C.
(Clarkson College of Technology Potsdam, N.Y., United States)
Burnell, J. F.
(Bell Telephone Laboratories, Inc. Whippany, N.J., United States)
Date Acquired
August 10, 2013
Publication Date
January 1, 1980
Publication Information
Publication: IEEE Transactions on Communications
Volume: COM-28
Subject Category
Space Communications, Spacecraft Communications, Command And Tracking
Accession Number
80A24152
Funding Number(s)
CONTRACT_GRANT: NSG-3191
Distribution Limits
Public
Copyright
Other

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