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Norton-Thevenin Receptance Coupling (NTRC) as a Payload Analysis ToolPresentation Agenda: Typical Payload Development Process, Problem, Solution Requirements, Methodology, Time Domain Solution, Launch Vehicle FEM, Heavy Payload FEM, Problem Size Comparison, Frequency Domain Validation, Time Domain Validation
Document ID
20180003339
Acquisition Source
Goddard Space Flight Center
Document Type
Presentation
Authors
Kaufman, Daniel S. (NASA Goddard Space Flight Center Greenbelt, MD, United States)
Gordon, Scott (NASA Goddard Space Flight Center Greenbelt, MD, United States)
Majed, Arya (Applied Structural Dynamics, Inc. (ASD) Houston, TX, United States)
Date Acquired
June 4, 2018
Publication Date
May 31, 2018
Subject Category
Launch Vehicles And Launch Operations
Report/Patent Number
GSFC-E-DAA-TN56061
Meeting Information
Meeting: European Conference on Spacecraft Structures, Materials & Environmental Testing (ECSSMET)
Location: Noordwijk
Country: Netherlands
Start Date: May 28, 2018
End Date: June 1, 2018
Sponsors: European Space Agency. European Space Research and Technology Center, ESTEC
Distribution Limits
Public
Copyright
Use by or on behalf of the US Gov. Permitted.
Keywords
NTRC

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