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Longitudinal and lateral-directional static aerodynamic characteristics of an unpowered escape system extraction rocket model with attached launch tubesAn escape system extraction rocket proposed for use on the Rotor Systems Research Aircraft was tested at Mach numbers of 0.1 and 0.3 through an angle of attack range from -2 deg to 102 deg and an angle of sideslip range from 0 deg to 15 deg in the Langley 7- by 10-foot high speed tunnel. The data are presented without analysis.
Document ID
19770020139
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Huffman, J. K. (NASA Langley Research Center Hampton, VA, United States)
Fox, C. H., Jr. (NASA Langley Research Center Hampton, VA, United States)
Satterthwaite, R. E. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 3, 2013
Publication Date
May 1, 1977
Subject Category
Air Transportation And Safety
Report/Patent Number
NASA-TM-X-74012
Report Number: NASA-TM-X-74012
Accession Number
77N27083
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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