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Supersonic aerodynamic characteristics of a Sparrow 3 type missile model with wing controls and comparison with existing tail-control resultsAn experimental investigation was conducted on a model of a wing control version of the Sparrow III type missile to determine the static aerodynamic characteristics over an angle of attack range from 0 deg to 40 deg for Mach numbers from 1.50 to 4.60.
Document ID
19780004098
Acquisition Source
Legacy CDMS
Document Type
Technical Publication (TP)
Authors
Monta, W. J. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 3, 2013
Publication Date
November 1, 1977
Subject Category
Aerodynamics
Report/Patent Number
NASA-TP-1078
L-11715
Report Number: NASA-TP-1078
Report Number: L-11715
Accession Number
78N12041
Funding Number(s)
PROJECT: RTOP 505-11-22-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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