NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Magnetic suspension options for spacecraft inertia-wheel applicationsDesign criteria for spacecraft inertia-wheel suspensions are listed. The advantages of magnetic suspensions over other suspension types for spacecraft inertia-wheel applications are cited along with the functions performed by magnetic suspension. The common designs for magnetic suspensions are enumerated. Materials selection of permanent magnets and core materials is considered.
Document ID
19850005562
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Downer, J. R.
(Draper (Charles Stark) Lab., Inc. Cambridge, MA, United States)
Date Acquired
August 12, 2013
Publication Date
November 1, 1984
Publication Information
Publication: NASA. Langley Research Center An Assessment of Integrated Flywheel System Technol.
Subject Category
Spacecraft Propulsion And Power
Accession Number
85N13871
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available