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Stability and control characteristics at Mach numbers from 0.20 to 4.63 of a cruciform air-to-air missile with triangular canard controls and a trapezoidal wing

Title:Stability and control characteristics at Mach numbers from 0.20 to 4.63 of a cruciform air-to-air missile with triangular canard controls and a trapezoidal wing
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Note:National Aeronautics and Space Administration ;, 1974
  
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Subject:Guided missiles -- Aerodynamics -- Statistics
Subject:Guided missiles -- Control systems -- Statistics
Subject:Guided missiles -- Stability -- Statistics
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