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Multiaxis control power from thrust vectoring for a supersonic fighter aircraft model at Mach 0.20 to 2.47

Title:Multiaxis control power from thrust vectoring for a supersonic fighter aircraft model at Mach 0.20 to 2.47
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Note:National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1987
  
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Subject:Airplanes -- Motors -- Thrust -- Statistics
Subject:Fighter planes
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