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Integrated Software for Analyzing Designs of Launch VehiclesLaunch Vehicle Analysis Tool (LVA) is a computer program for preliminary design structural analysis of launch vehicles. Before LVA was developed, in order to analyze the structure of a launch vehicle, it was necessary to estimate its weight, feed this estimate into a program to obtain pre-launch and flight loads, then feed these loads into structural and thermal analysis programs to obtain a second weight estimate. If the first and second weight estimates differed, it was necessary to reiterate these analyses until the solution converged. This process generally took six to twelve person-months of effort. LVA incorporates text to structural layout converter, configuration drawing, mass properties generation, pre-launch and flight loads analysis, loads output plotting, direct solution structural analysis, and thermal analysis subprograms. These subprograms are integrated in LVA so that solutions can be iterated automatically. LVA incorporates expert-system software that makes fundamental design decisions without intervention by the user. It also includes unique algorithms based on extensive research. The total integration of analysis modules drastically reduces the need for interaction with the user. A typical solution can be obtained in 30 to 60 minutes. Subsequent runs can be done in less than two minutes.
Document ID
20110024117
Acquisition Source
Marshall Space Flight Center
Document Type
Other - NASA Tech Brief
Authors
Philips, Alan D.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
August 25, 2013
Publication Date
August 1, 2003
Publication Information
Publication: NASA Tech Briefs, August 2003
Subject Category
Launch Vehicles And Launch Operations
Report/Patent Number
MFS-31694
Report Number: MFS-31694
Distribution Limits
Public
Copyright
Public Use Permitted.
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