Actions for Aerodynamic results of a separation effects test (IA87) on a 0.01-scale model (52-OTS) of the integrated SSV in the AEDC

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Aerodynamic results of a separation effects test (IA87) on a 0.01-scale model (52-OTS) of the integrated SSV in the AEDC/VKF 40-by-40 inch supersonic wind tunnel A, volume 2.

Author
Campbell, J. H., II
Published
Jun 1, 1975.
Physical Description
1 electronic document
Online Version

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Restrictions on Access
Unclassified, Unlimited, Publicly available.
Free-to-read Unrestricted online access
Summary
Data tables, model figures, and tabulated source data are given for aerodynamic investigations of separation effects in the integrated space shuttle vehicle. For Volume 1, see N75-28101.
Other Subject(s)
Collection
NASA Technical Reports Server (NTRS) Collection.
Note
Document ID: 19750022161.
Accession ID: 75N30234.
DMS-DR-2192-VOL-2.
NASA-CR-141542.
Terms of Use and Reproduction
No Copyright.
View MARC record | catkey: 15738984