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Development and correlation: Viking Orbiter analytical dynamic model with modal testThe Viking Orbiter (VO) experience in the achievement of a mathematical model is described along with the following project activities: (1) the generation of the overall plan for load analysis, an analytical dynamic model, and development tests; (2) the performance of VO subsystem static and modal tests; and (3) the correlation of the VO system model analysis and test. Success is attributed to the coordination of analysis and test using substructure modal coupling techniques.
Document ID
19740020220
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Wada, B. K.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Garba, J. A.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Chen, J. C.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
September 3, 2013
Publication Date
June 1, 1974
Subject Category
Space Vehicles
Report/Patent Number
NASA-CR-138728
JPL-TM-33-690
Report Number: NASA-CR-138728
Report Number: JPL-TM-33-690
Accession Number
74N28333
Funding Number(s)
CONTRACT_GRANT: NAS7-100
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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