NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Analysis of payload bay magnetic fields due to dc power multipoint and single point ground configurationsAn analysis of magnetic fields in the Orbiter Payload Bay resulting from the present grounding configuration (structure return) was presented and the amount of improvement that would result from installing wire returns for the three dc power buses was determined. Ac and dc magnetic fields at five points in a cross-section of the bay are calculated for both grounding configurations. Y and Z components of the field at each point are derived in terms of a constant coefficient and the current amplitude of each bus. The dc loads assumed are 100 Amperes for each bus. The ac noise current used is a spectrum 6 db higher than the Orbiter equipment limit for narrowband conducted emissions. It was concluded that installing return wiring to provide a single point ground for the dc Buses in the Payload Bay would reduce the ac and dc magnetic field intensity by approximately 30 db.
Document ID
19760016259
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Lawton, R. M.
(McDonnell-Douglas Technical Services Co., Inc. Houston, TX, United States)
Date Acquired
September 3, 2013
Publication Date
April 28, 1976
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
NASA-CR-147703
REPT-1.3-DN-C0504-030
Report Number: NASA-CR-147703
Report Number: REPT-1.3-DN-C0504-030
Accession Number
76N23347
Funding Number(s)
CONTRACT_GRANT: NAS9-14960
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available