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Nike Black Brant V high altitude dynamic instability characteristicsFlight experience on the Nike Black Brant V has demonstrated the existence of plume induced flow separation over the fins and aft body of the Black Brant V motor. Modelling of the forces associated with this phenomenon as well as analysis of the resultant vehicle coning motion and its effect on the velocity vector heading are presented. A summary of Nike Black Brant V flight experience with high altitude dynamic instability is included.
Document ID
19790041756
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Authors
Montag, W. H.
(Management and Technical Services Co. Beltsville, MD, United States)
Walker, L. L., Jr.
(Management and Technical Services Co. Beltsville, Md., United States)
Date Acquired
August 9, 2013
Publication Date
January 1, 1979
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
AIAA PAPER 79-0507
Meeting Information
Meeting: Sounding Rocket Technology Conference
Location: Houston, TX
Start Date: March 7, 1979
End Date: March 9, 1979
Accession Number
79A25769
Funding Number(s)
CONTRACT_GRANT: NAS5-23551
CONTRACT_GRANT: NAS5-25182
Distribution Limits
Public
Copyright
Other

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