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Mach 6 experimental and theoretical stability and performance of a cruciform missile at angles of attack up to 65⁰

Title:Mach 6 experimental and theoretical stability and performance of a cruciform missile at angles of attack up to 65⁰
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Note:National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1987
  
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Subject:Aerodynamics, Hypersonic
Subject:Guided missiles -- Aerodynamics
Subject:Guided missiles -- Control systems
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