Structural Design Criteria Applicable to a Space Shuttle
Author :
Publisher :
Page : 112 pages
File Size : 11,22 MB
Release : 1972
Category : Reusable space vehicles
ISBN :
Author :
Publisher :
Page : 112 pages
File Size : 11,22 MB
Release : 1972
Category : Reusable space vehicles
ISBN :
Author : Robert Samuel Ryan
Publisher :
Page : 136 pages
File Size : 29,58 MB
Release : 1981
Category :
ISBN :
Author : Robert Samuel Ryan
Publisher :
Page : 104 pages
File Size : 24,77 MB
Release : 1989
Category : Space vehicles
ISBN :
Author :
Publisher :
Page : 104 pages
File Size : 40,13 MB
Release : 1989
Category : Science
ISBN :
Author : R. Ryan
Publisher :
Page : 120 pages
File Size : 10,60 MB
Release : 1996
Category : Astronautics
ISBN :
Author : J. C. Blair
Publisher :
Page : 264 pages
File Size : 18,1 MB
Release : 2001
Category :
ISBN :
Author : United States. National Aeronautics and Space Administration
Publisher :
Page : 108 pages
File Size : 15,1 MB
Release : 1989
Category : Aeronautics
ISBN :
Author :
Publisher :
Page : 132 pages
File Size : 13,32 MB
Release : 1981
Category : Reusable space vehicles
ISBN :
Author : Ahmed Khairy Noor
Publisher : AIAA
Page : 544 pages
File Size : 42,2 MB
Release : 1998
Category : Technology & Engineering
ISBN : 9781563471162
Drawn from early volumes of Aerospace America and its antecedents, this book rescues the insights, concerns, and dreams of dozens of structural engineers for the next generation of aerospace scientists and engineers. Written by eminent individuals in structures, this book provides accessible source material for university-level design courses in aerospace engineering. The first paper in Structures Technology deals with new structures for future aerospace systems and provides a contrast between our current thinking and past technology plans. Succeeding papers are historical reports covering materials and structures, general structures technology, aircraft structures, space structures, and structural dynamics technology. You will also find sections covering structural configurations, thermal protection systems, subsonic aircraft, supersonic and hypersonic vehicles and structures for space systems.
Author : V. Deriugin
Publisher :
Page : 292 pages
File Size : 29,55 MB
Release : 1972
Category : Aerodynamic heating
ISBN :
A study was conducted to determine methodology for combining thermal structural loads and assessing the effects of the combined loads on the design of a thermal protection system and a hot structure of a high cross range delta wing space shuttle orbiter vehicle. The study presents guidelines for establishing a basis for predicting thermal and pressure environments and for determining limit and ultimate design loads on the vehicle during reentry. Limit trajectories were determined by using dispersions on a representative nominal mission and system parameters expected during the life of the vehicle. Nine chosen locations on the vehicle surface having TPS or hot structures were examined, and weight sensitivity analyses were performed for each location.