Wind Tunnel Force Tests of Saturn V Configurations at Supersonic Mach Numbers PDF Download
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Author: Neil Arthur Zarin
Publisher:
ISBN:
Category : Saturn launch vehicles
Languages : en
Pages : 94
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Author: Neil Arthur Zarin
Publisher:
ISBN:
Category : Saturn launch vehicles
Languages : en
Pages : 94
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Author: David R. Carlson
Publisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 76
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The static stability and axial force characteristics of an upper stage Saturn IB/Apollo model were investigated in a series of wind tunnel tests at Mach numbers between 1.93 and 8.05. This report presents and analyzes the results of these small scale studies. Test procedures and models are described, and consideration of boundary layer characteristics and violated modeling rules yields an assessment of the validity of the data Four basic models provided evaluation of the basic launch vehicle characteristics, as well as the effects of two modes of mission abort and jettison of the launch escape system. The launch configuration experienced sudden, strong changes in stability derivatives and axial force coefficients near Mach 5. No similar changes were observed on the other configurations. Effects of Reynolds number, Mach number, and boundary layer trips were obtained for each shape. The faired curves are believed to be valid for full-scale flight of the Saturn IB/Apollo upper stage.
Author: Dennis E. Fuller
Publisher:
ISBN:
Category : Launch vehicles (Astronautics)
Languages : en
Pages : 40
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Author:
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 780
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Author: Maurice A. Sylvester
Publisher:
ISBN:
Category : Launch vehicles (Astronautics)
Languages : en
Pages : 54
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Wind tunnel force tests were performed on a scale model of the Mercury Redstone. The model consisted of the Redstone booster section and the Mercury capsule without the escape rocket pylon. The static stability and drag characteristics of this configuration were determined at Mach numbers from 2.00 to 5.00 and at angles of attack from -4 to 12 degrees. The results are summarized and discussed at zero angle of attack. (Author).
Author:
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ISBN:
Category : Aeronautics
Languages : en
Pages : 974
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Book Description
Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.
Author: Roger H. Fournier
Publisher:
ISBN:
Category :
Languages : en
Pages : 28
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Author: Frederick C. Grant
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ISBN:
Category :
Languages : en
Pages : 108
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Author: Earl J. Montoya
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ISBN:
Category :
Languages : en
Pages : 76
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Author: William C. Moseley (Jr.)
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 76
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