NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Press Enter or click the Search button to begin your search.

Back to Results
Internal electrostatic discharge hazard risk assessment to the Galileo orbiterA worst case assessment was performed on the Command Data System (CDS) multilayer printed circuit board and an output power transformer module in the power subsystem. An estimate of the Jovian environment during the 35 hour orbit insertion was supplied by JPL and used as an input to calculate the electron transport into the Galileo components. A radiation shielding analysis computer code, CHARGE, calculated the electron transport deposition trapped in the anticipated sensitive areas of the multilayer board and transformer module. Based on these trapped charge calculations electric fields were calculated between the identified isolated areas and the spacecraft ground. The results of the assessment of electrostatic discharge (DSD) in the CDS multilayer printed circuit board indicate that the probability of ESD in the FR4 is low. The probability of ESD in the components attached to the multilayer board, however, is uncertain based on a lack of prior experimental data.
Document ID
19810008593
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Schmidt, R. E.
(General Electric Co. Philadelphia, PA, United States)
Andrews, J. C.
(General Electric Co. Philadelphia, PA, United States)
Treadaway, M. J.
(JAYCOR)
Leadon, R. E.
(JAYCOR)
Date Acquired
September 4, 2013
Publication Date
October 27, 1980
Subject Category
Launch Vehicles And Space Vehicles
Report/Patent Number
NASA-CR-163930
Report Number: NASA-CR-163930
Accession Number
81N17113
Funding Number(s)
CONTRACT_GRANT: JPL-955785
CONTRACT_GRANT: NAS7-100
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available