My Account Log in

2 options

Preliminary in-flight loads analysis of in-line launch vehicles using the VLOADS 1.4 program / J.B. Graham and P.L. Luz.

Online

Available online

View online

U.S. Government Documents Available online

View online
Format:
Book
Government document
Author/Creator:
Graham, J. B. (Jerry B.), author.
Luz, P.L., author.
Contributor:
George C. Marshall Space Flight Center, issuing body.
Series:
NASA technical memorandum ; 1998-208472.
NASA/TM ; 1998-208472
Language:
English
Genre:
Technical Memorandum
Physical Description:
1 online resource (vii, 46 pages) : illustrations.
Other Title:
Preliminary in-flight loads analysis of in-line launch vehicles using the Vehicle Loads 1.4 program
Place of Publication:
Huntsville, Alabama : National Aeronautics and Space Administration, Marshall Space Flight Center, June 1998.
Summary:
To 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 workbook 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
Notes:
"June 1998."
"Performing organization: George C. Marshall Space Flight Center"--Report documentation page.
Includes bibliographical references (page 46).
Description based on online resource; title from PDF title page (NASA, viewed July 31, 2017).
Other Format:
Print version: Preliminary in-flight loads analyses of in-line launch vehicles using the vloads 1.4 program
Microfiche version: Graham, J. B. (Jerry B.). Preliminary in-flight loads analysis of in-line launch vehicles using the VLOADS 1.4 program
OCLC:
703645510

The Penn Libraries is committed to describing library materials using current, accurate, and responsible language. If you discover outdated or inaccurate language, please fill out this feedback form to report it and suggest alternative language.

Find

Home Release notes

My Account

Shelf Request an item Bookmarks Fines and fees Settings

Guides

Using the Find catalog Using Articles+ Using your account