NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login

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

Back to Results
A modal model for SCOLE structural dynamicsInformation on a modal model for the Spacecraft Control Laboratory (SCOLE) is given in viewgraph form. A partial differential equation model covering roll bending, pitch bending, torsion, shear forces, and bending moments is given.
Document ID
19920074940
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Joshi, Suresh M. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 15, 2013
Publication Date
January 1, 1984
Publication Information
Publication: Spacecraft Control Laboratory Experiment (SCOLE) Workshop, 1984
Subject Category
Spacecraft Design, Testing And Performance
Accession Number
92N70064
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Document Inquiry

Available Downloads

There are no available downloads for this record.

Related Records

There are no records associated with this record.
No Preview Available