NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Research on the structural dynamics verification of flexible spacecraftLangley spacecraft structural dynamics research based on a broad range of experimental and analytical studies, which contributed to the technology base for designing and building advanced spacecraft structures, is reviewed. It is concluded that considerable progress has been made toward developing the scale model technology for validating mathematical models used to predict the on-orbit dynamic behavior of spacecraft structures. Advanced suspension systems for testing models of spacecraft as well as feasibility of using modal data to detect damage in truss-type structures were demonstrated.
Document ID
19930068194
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Kvaternik, Raymond G.
(NASA Langley Research Center Hampton, VA, United States)
Hanks, Brantley R.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 16, 2013
Publication Date
March 1, 1993
Subject Category
Launch Vehicles And Space Vehicles
Meeting Information
Meeting: Inst. of Environmental Sciences and Aerospace Corp., Aerospace Testing Seminar
Location: Manhattan Beach, CA
Country: United States
Start Date: March 9, 1993
End Date: March 11, 1993
Sponsors: Aerospace Corp., Inst. of Environmental Sciences
Accession Number
93A52191
Distribution Limits
Public
Copyright
Other

Available Downloads

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