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Spacecraft subsystem checkout by minicomputerThe minicomputer, with its large capacity in a small and inexpensive package, can be an important component in special-purpose test equipment. The Voyager spacecraft flight data subsystem support equipment is an example of computer-based test gear. The subsystem to be tested is a major control and data acquisition element of the Voyager spacecraft, with a large number of interfaces to several other onboard subsystems. This equipment was designed to meet spacecraft subsystem testing requirements while making maximum use of off-the-shelf commercial components. Careful consideration was given to design tradeoffs in the areas of commercial versus specially built hardware and hardware versus software problem solutions. The resulting system is an integrated package of commercial and special-purpose hardware plus software.
Document ID
19790031637
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Andersen, R. W.
(California Institute of Technology, Jet Propulsion Laboratory, Pasadena Calif., United States)
Date Acquired
August 9, 2013
Publication Date
November 1, 1977
Subject Category
Ground Support Systems And Facilities (Space)
Meeting Information
Meeting: Institute of Electrical and Electronics Engineers and Electronic Representatives Association, Electronic Show and Convention
Location: Chicago, IL
Start Date: November 8, 1977
End Date: November 10, 1977
Sponsors: Institute of Electrical and Electronics Engineers, Electronic Representatives Association
Accession Number
79A15650
Funding Number(s)
CONTRACT_GRANT: NAS7-100
Distribution Limits
Public
Copyright
Other

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