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Orbiter CCTV video signal noise analysisThe amount of steady state and transient noise which will couple to orbiter CCTV video signal wiring is predicted. The primary emphasis is on the interim system, however, some predictions are made concerning the operational system wiring in the cabin area. Noise sources considered are RF fields from on board transmitters, precipitation static, induced lightning currents, and induced noise from adjacent wiring. The most significant source is noise coupled to video circuits from associated circuits in common connectors. Video signal crosstalk is the primary cause of steady state interference, and mechanically switched control functions cause the largest induced transients.
Document ID
19770022405
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Lawton, R. M.
(McDonnell-Douglas Astronautics Co. Houston, TX, United States)
Blanke, L. R.
(McDonnell-Douglas Astronautics Co. Houston, TX, United States)
Pannett, R. F.
(McDonnell-Douglas Astronautics Co. Houston, TX, United States)
Date Acquired
September 3, 2013
Publication Date
August 5, 1977
Subject Category
Communications And Radar
Report/Patent Number
NASA-CR-151479
REPT-1.3-DN-C0704-039
Report Number: NASA-CR-151479
Report Number: REPT-1.3-DN-C0704-039
Accession Number
77N29349
Funding Number(s)
CONTRACT_GRANT: NAS9-14960
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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