Preliminary Analysis and Design Optimization of the Short Spacer Truss of Space Station Freedom
Author : A. S. Gendy
Publisher :
Page : 24 pages
File Size : 13,44 MB
Release : 1993
Category : Trusses
ISBN :
Author : A. S. Gendy
Publisher :
Page : 24 pages
File Size : 13,44 MB
Release : 1993
Category : Trusses
ISBN :
Author : Sasan C. Armand
Publisher :
Page : 20 pages
File Size : 35,97 MB
Release : 1992
Category : Large space structures (Astronautics)
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Author :
Publisher :
Page : 836 pages
File Size : 18,82 MB
Release : 1994
Category : Aeronautics
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Author :
Publisher :
Page : 872 pages
File Size : 41,98 MB
Release : 1994-08
Category : Government publications
ISBN :
Author : Atef S. Gendy
Publisher :
Page : 28 pages
File Size : 49,58 MB
Release : 1995
Category : Parallel programming (Computer science)
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Author :
Publisher :
Page : pages
File Size : 36,94 MB
Release : 1994
Category : Government publications
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Author : National Aeronautics and Space Administration (NASA)
Publisher : Createspace Independent Publishing Platform
Page : 34 pages
File Size : 45,29 MB
Release : 2018-08-16
Category :
ISBN : 9781725639850
Here, the focus is on the design and configuration feasibility of the short spacer for the Space Station Program in its launch configuration. The product of this study is being used by Rockwell International (Rocketdyne Division) as they continue their design concept of the current short spacer configuration. It is anticipated that the launch loads will dominate the on-orbit loads and dictate the design configuration of the short spacer. At the present time, the on-orbit loads have not been generated. The structural analysis discussed herein is based on the transient events derived from the Space Transportation System (STS) Interface Control Document (ICD). The transient loading events consist of liftoff loads, landing loads, and emergency landing loads. The quasi-static loading events have been neglected, since the magnitude of the acceleration factors are lower than the transient acceleration factors. The normal mode analyses presented herein are based on the most feasible configurations with acceptable stress ranges. Armand, Sasan C. and Dohogne, Caroline A. Glenn Research Center NASA-TM-105558, E-6882, NAS 1.15:105558 RTOP 474-46-10...
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Page : 1686 pages
File Size : 46,39 MB
Release : 199?
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Author : Surya N. Patnaik
Publisher :
Page : 20 pages
File Size : 11,16 MB
Release : 1994
Category : Linear programming
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Author : Robert G. Chamberlain
Publisher :
Page : pages
File Size : 38,40 MB
Release : 1990
Category :
ISBN :