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

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

Author
Martin, T. A.
Published
Oct 12, 1973.
Physical Description
1 electronic document
Additional Creators
Spring, D. J.
Online Version

Availability

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Restrictions on Access
Unclassified, Unlimited, Publicly available.
Free-to-read Unrestricted online access
Summary
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. Data are presented showing the interference created by the rear mounted reaction control system. Two candidate fins were installed on the model during tests: a flat folding fin and a curved wrap around fin.
Other Subject(s)
Collection
NASA Technical Reports Server (NTRS) Collection.
Note
Document ID: 19750002949.
Accession ID: 75N11021.
AD-784121.
RD-73-27.
NASA-CR-140750.
Terms of Use and Reproduction
No Copyright.
View MARC record | catkey: 15742220