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Investigation of space shuttle launch vehicle external tank nose configuration effects (model 67-OTS) in the Rockwell International 7 by 7 foot trisonic wind tunnel (IA69)

By Mennell, R.

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Book Id: WPLBN0002203812
Format Type: PDF eBook :
File Size: 8.1 MB
Reproduction Date: 2012
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Title: Investigation of space shuttle launch vehicle external tank nose configuration effects (model 67-OTS) in the Rockwell International 7 by 7 foot trisonic wind tunnel (IA69)  
Author: Mennell, R.
Volume:
Language: English
Subject: COMPTON EFFECT, PARTICLE DENSITY (CONCENTRATION), NONRELATIVISTIC MECHANICS
Collections: NASA Publication Collection
Historic
Publication Date:
1974
Publisher:

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R, M., & R, R. (1974). Investigation of space shuttle launch vehicle external tank nose configuration effects (model 67-OTS) in the Rockwell International 7 by 7 foot trisonic wind tunnel (IA69). Retrieved from http://nationalpubliclibrary.info/


Description
Supplemental catalog subcollection information: NASA Publication Collection; Astrophysics and Technical Documents; Wind tunnel aerodynamic investigations were conducted on an 0.015-scale representation of the space shuttle launch configuration. The primar

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: COMPTON EFFECT; PARTICLE DENSITY (CONCENTRATION); NONRELATIVISTIC MECHANICS; LORENTZ TRANSFORMATIONS; ANISOTROPY; ISOTROPY; SOLAR WIND

 

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