Actions for A WIND-TUNNEL INVESTIGATION aT SUBSONIC aND LOW SUPERSONIC SPEEDS oF a RE-ENTRY VEHICLE WITH RETRACTABLE WINGS

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A WIND-TUNNEL INVESTIGATION aT SUBSONIC aND LOW SUPERSONIC SPEEDS oF a RE-ENTRY VEHICLE WITH RETRACTABLE WINGS

Author
Smith, W. G.
Published
Feb 1, 1961.
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
Wind tunnel tests of blunt reentry vehicle with retractable wings
Other Subject(s)
Collection
NASA Technical Reports Server (NTRS) Collection.
Note
Document ID: 19630004028.
Accession ID: 63N13904.
NASA-TM-X-398.
Terms of Use and Reproduction
No Copyright.
View MARC record | catkey: 15437602