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Preliminary In-Flight Loads Analysis of In-Line Launch Vehicles using the VLOADS 1.4 ProgramTo calculate structural loads of in-line launch vehicles for preliminary design, a very useful computer program is VLOADS 1.4. This software may also be used to calculate structural loads for upper stages and planetary transfer vehicles. Launch vehicle inputs such as aerodynamic coefficients, mass properties, propellants, engine thrusts, and performance data are compiled and analyzed by VLOADS to produce distributed shear loads, bending moments, axial forces, and vehicle line loads as a function of X-station along the vehicle's length. Interface loads, if any, and translational accelerations are also computed. The major strength of the software is that it enables quick turnaround analysis of structural loads for launch vehicles during the preliminary design stage of its development. This represents a significant improvement over the alternative-the time-consuming, and expensive chore of developing finite element models. VLOADS was developed as a Visual BASIC macro in a Microsoft Excel 5.0 work book on a Macintosh. VLOADS has also been implemented on a PC computer using Microsoft Excel 7.0a for Windows 95. VLOADS was developed in 1996, and the current version was released to COSMIC, NASA's Software Technology Transfer Center, in 1997. The program is a copyrighted work with all copyright vested in NASA.
Document ID
19980201045
Document Type
Technical Memorandum (TM)
Authors
Graham, J. B. (NASA Marshall Space Flight Center Huntsville, AL United States)
Luz, P. L. (NASA Marshall Space Flight Center Huntsville, AL United States)
Date Acquired
September 6, 2013
Publication Date
June 1, 1998
Subject Category
Computer Programming and Software
Report/Patent Number
M-873
NASA/TM-1998-208472
NAS 1.15:208472
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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