Static Stability and Axial Force Characteristics of a 1.32 Percent Scale Model of the Saturn I B/ APOLLO, Its Components, and the Saturn I B/ APOLLO/ Minuteman Launch Vehicle, Determined by Wind Tunnel Test
1965
100 pages
Report
Keine Angabe
Englisch
Aerodynamics , Apollo spacecraft , Minuteman icbm , Saturn ib launch vehicle , Wind tunnel stability test , Angle , Attack , Axial , Component , Data , Force , Instrumentation , Mach number , Model , Reduction , Reynolds number , Scale , Stability , Static , Test , Tunnel , Wind
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