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Wind-tunnel investigation at Mach numbers from 0.60 to 1.20 of the static aerodynamic characteristics of a model of a possible nonlifting reentry capsule in combination with a rocket booster

Title:Wind-tunnel investigation at Mach numbers from 0.60 to 1.20 of the static aerodynamic characteristics of a model of a possible nonlifting reentry capsule in combination with a rocket booster
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Note:National Aeronautics and Space Administration, 1960
  
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Subject:Aerodynamics -- Testing
Subject:Jet fighter planes -- Wind tunnel testing
Subject:Mach number -- Testing
Subject:Statics -- Testing
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