NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Development and implementation of the verification process for the shuttle avionics systemThe background of the shuttle avionics system design and the unique drivers associated with the redundant digital multiplexed data processing system are examined. With flight software pervading to the lowest elements of the flight critical subsystems, it was necessary to identify a unique and orderly approach of verifying the system as flight ready for STS-1. The approach and implementation plan is discussed, and both technical problems and management issues are dealt with.
Document ID
19850008587
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Smith, H. E.
(NASA Lyndon B. Johnson Space Center Houston, TX, United States)
Fouts, W. B.
(Rockwell International Corp. Downey, Calif., United States)
Mesmer, J.
(Rockwell International Corp. Downey, Calif., United States)
Date Acquired
August 12, 2013
Publication Date
January 1, 1985
Publication Information
Publication: Space Shuttle Tech. Conf., Pt. 1
Subject Category
Aircraft Instrumentation
Accession Number
85N16896
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available