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The engineering design integration (EDIN) systemA digital computer program complex for the evaluation of aerospace vehicle preliminary designs is described. The system consists of a Univac 1100 series computer and peripherals using the Exec 8 operating system, a set of demand access terminals of the alphanumeric and graphics types, and a library of independent computer programs. Modification of the partial run streams, data base maintenance and construction, and control of program sequencing are provided by a data manipulation program called the DLG processor. The executive control of library program execution is performed by the Univac Exec 8 operating system through a user established run stream. A combination of demand and batch operations is employed in the evaluation of preliminary designs. Applications accomplished with the EDIN system are described.
Document ID
19750009046
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Glatt, C. R.
(Aerophysics Research Corp. Houston, TX, United States)
Hirsch, G. N.
(Aerophysics Research Corp. Houston, TX, United States)
Alford, G. E.
(Aerophysics Research Corp. Houston, TX, United States)
Colquitt, W. N.
(Aerophysics Research Corp. Houston, TX, United States)
Reiners, S. J.
(Aerophysics Research Corp. Houston, TX, United States)
Date Acquired
September 3, 2013
Publication Date
December 1, 1974
Subject Category
Computer Programming And Software
Report/Patent Number
NASA-CR-141598
Report Number: NASA-CR-141598
Accession Number
75N17118
Funding Number(s)
CONTRACT_GRANT: NAS9-13584
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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