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Static stability and drag characteristics of the HAST missile at Mach numbers 2.25, 3.0, and 4.0

Title:Static stability and drag characteristics of the HAST missile at Mach numbers 2.25, 3.0, and 4.0
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Note:Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1974., 1974
  
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Subject:Drag (Aerodynamics)
Subject:Guided missiles -- Aerodynamics
Subject:Guided missiles -- Testing
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