NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login

Press Enter or click the Search button to begin your search.

Back to Results
Large-scale wind-tunnel tests of three vehicles incorporating a deployable rigid wingWind-tunnel tests were performed to determine the aerodynamic characteristics of three full-scale vehicles incorporating a unique folding metal wing, and to investigate its deployment characteristics. The static aerodynamic data are presented without analysis.
Document ID
19750016599
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Feistel, T. W. (NASA Ames Research Center Moffett Field, CA, United States)
Maki, R. L. (NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 3, 2013
Publication Date
August 1, 1974
Subject Category
Aeronautics (General)
Report/Patent Number
A-5854
NASA-TM-X-62405
Report Number: A-5854
Report Number: NASA-TM-X-62405
Accession Number
75N24671
Funding Number(s)
PROJECT: RTOP 505-11-21
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

Related Records

There are no records associated with this record.
No Preview Available