NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
System design aspects and flight experience of the electrical interfaces across the Galileo spacecraft spin bearing assemblyThe Galileo spacecraft design uses a dual-spin general configuration with spun and despun sections; the mechanical connection between the two sections is accomplished by means of a spin bearing assembly (SBA) whose electrical interfacing uses both slip rings/brushes and rotary transformers that are located within the SBA. Attention is presently given to the design features of the SBA, the electrical interface flight anomaly and investigation experience with Galileo to date, and the responses of the Galileo Flight Team to those anomalies.
Document ID
19930046993
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Landano, Matthew R.
(JPL Pasadena, CA, United States)
Date Acquired
August 16, 2013
Publication Date
February 1, 1993
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
AIAA PAPER 93-1106
Meeting Information
Meeting: AIAA, AHS, and ASEE, Aerospace Design Conference
Location: Irvine, CA
Country: United States
Start Date: February 16, 1993
End Date: February 19, 1993
Sponsors: AHS, ASEE, AIAA
Accession Number
93A30990
Distribution Limits
Public
Copyright
Other

Available Downloads

There are no available downloads for this record.
No Preview Available