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Static aerodynamic characteristics of three rocket-vehicle configurations at Mach numbers from 1.80 to 4.63 including some effects of fin size, fin cant, and auxiliary rocket motors

Title:Static aerodynamic characteristics of three rocket-vehicle configurations at Mach numbers from 1.80 to 4.63 including some effects of fin size, fin cant, and auxiliary rocket motors
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Note:National Aeronautics and Space Administration, 1963
  
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Subject:Aerodynamics, Supersonic -- Statistics
Subject:Rocket engines -- Statistics
Subject:Rockets (Aeronautics) -- Fins -- Statistics
Subject:Stability of rockets -- Statistics
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