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Wind tunnel test results for the direction controlled antitank DCAT missile at Mach numbers from 0.64 to 2.50

By Martin, T. A.

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Book Id: WPLBN0002203641
Format Type: PDF eBook :
File Size: 11.3 MB
Reproduction Date: 2012
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Title: Wind tunnel test results for the direction controlled antitank DCAT missile at Mach numbers from 0.64 to 2.50  
Author: Martin, T. A.
Volume:
Language: English
Subject: GEODESY, GEODETIC SATELLITES, OCEAN SURFACE
Collections: NASA Publication Collection
Historic
Publication Date:
1973
Publisher:

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A, M. T., & J, S. D. (1973). Wind tunnel test results for the direction controlled antitank DCAT missile at Mach numbers from 0.64 to 2.50. Retrieved from http://worldlibrary.in/


Description
Supplemental catalog subcollection information: NASA Publication Collection; Astrophysics and Technical Documents; Wind tunnel test results are presented to show aerodynamic characteristics over the Mach number range of 0.64 to 2.50 of the DCAT missile. D

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: GEODESY; GEODETIC SATELLITES; OCEAN SURFACE; GROUND TRUTH; OCEANOGRAPHY; GEOIDS; PROBLEM SOLVING; TECHNOLOGY UTILIZATION

 

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