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Wind tunnel test of the 0.010-scale space shuttle integrated vehicle in the NASA-Ames 3.5 foot hypersonic wind tunnel (IA10)

By Fitzgerald, F. F.

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Book Id: WPLBN0002202839
Format Type: PDF eBook :
File Size: 7.4 MB
Reproduction Date: 2012
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Title: Wind tunnel test of the 0.010-scale space shuttle integrated vehicle in the NASA-Ames 3.5 foot hypersonic wind tunnel (IA10)  
Author: Fitzgerald, F. F.
Volume:
Language: English
Subject: ACTUATORS, AIRCRAFT CONTROL, EQUIPMENT SPECIFICATIONS
Collections: NASA Publication Collection
Historic
Publication Date:
1973
Publisher:

Citation

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F, F. F., W, C. J., A, M. J., & T, P. M. (1973). Wind tunnel test of the 0.010-scale space shuttle integrated vehicle in the NASA-Ames 3.5 foot hypersonic wind tunnel (IA10). Retrieved from http://members.worldlibrary.net/


Description
Supplemental catalog subcollection information: NASA Publication Collection; Astrophysics and Technical Documents; Experimental aerodynamic investigations were conducted in the NASA Ames Research Center 3.5-Foot Hypersonic Wind Tunnel on a 0.010-scale mod

Summary
Contributor: National Aeronautics and Space Administration (NASA). The digitalization of this book was sponsored by National Aeronautics and Space Administration (NASA); Additional Subject Descriptions: ACTUATORS; AIRCRAFT CONTROL; EQUIPMENT SPECIFICATIONS; COST ANALYSIS; HYDRAULIC EQUIPMENT; SERVOMECHANISMS; MECHANICAL DEVICES

 

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