columbus · Methods in Structural Dynamics for Thin Shell Clustered Launch Vehicles

Methods in Structural Dynamics for Thin Shell Clustered Launch Vehicles

Title: Methods in Structural Dynamics for Thin Shell Clustered Launch Vehicles
Date: 1965
Index Abstract: Coming Soon
Photo Quality: Not Needed
Report Number: FDL TDR 64-105
Creator: Keith, J. S.; Lincoln, J. W.
Corporate Author: LTV Astronautics
Laboratory: Air Force Flight Dynamics Laboratory
Extent: 760
Identifier: AD0463571
Access Rights: Notice(s)
Distribution Classification: 1
Contract: AF 33(657)-9146
DoD Project: 1370
DoD Task: 137008
DTIC Record Exists: No
Distribution Change Authority Correspondence: AFFDL LTR
Abstract: A general methodology in Structural Dynamics based on the use of generalized coordinates is presented. These general methods are demonstrated by analysis of some of the problems of slender, conventional, launch vehicles. Applications of the general methodology are also given for complex configurations employing thin shell tanks in clustered arrangements. The methods of structural analysis and vibration analysis that are presented are not restricted to any particular geometry and apply to any complex redundantly coupled structure. To further demonstrate the general methods, a vibration analysis of the clustered Saturn I launch vehicle is presented.
Report Availability: Full text available
Date Issued: 1965-04
Provenance: Lockheed Martin Missiles & Fire Control
Type: report
Format: 1 online resource