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Longitudinal and lateral-directional static aerodynamic characteristics of an unpowered escape system extraction rocket modelAn 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.
Document ID
19770013081
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
March 1, 1977
Subject Category
Aerodynamics
Report/Patent Number
NASA-TM-X-74009
Report Number: NASA-TM-X-74009
Accession Number
77N20025
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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