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Effect on tail-fin span on stability and control characteristics of a canard-controlled missile at supersonic Mach numbers

Effect on tail-fin span on stability and control characteristics of a canard-controlled missile at supersonic Mach numbers

By A. B. Blair

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Publish Date

1983

Publisher

National Aeronautics and Space Administration, Scientific and Technical Information Branch,For sale by the National Technical Information Service]

Language

eng

Pages

83

1-3 of 3 Editions

Effect on tail-fin span on stability and control characteristics of a canard-controlled missile at supersonic Mach numbers

View Effect on tail-fin span on stability and control characteristics of a canard-controlled missile at supersonic Mach numbers
Effect on tail-fin span on stability and control characteristics of a canard-controlled missile at supersonic Mach numbers

Language: eng

Pages: 83

Published In: 1983

Publisher: National Aeronautics and Space Administration, Scientific and Technical Information Branch, For sale by the National Technical Information Service]

Effect on tail-fin span on stability and control characteristics of a canard-controlled missile at supersonic Mach numbers

View Effect on tail-fin span on stability and control characteristics of a canard-controlled missile at supersonic Mach numbers
Effect on tail-fin span on stability and control characteristics of a canard-controlled missile at supersonic Mach numbers

Language: eng

Pages: 83

Published In: 1983

Publisher: National Aeronautics and Space Administration, Scientific and Technical Information Branch, For sale by the National Technical Information Service]

Effect on tail-fin span on stability and control characteristics of a canard-controlled missile at supersonic Mach numbers

View Effect on tail-fin span on stability and control characteristics of a canard-controlled missile at supersonic Mach numbers
Effect on tail-fin span on stability and control characteristics of a canard-controlled missile at supersonic Mach numbers

Language: eng

Pages: 83

Published In: 1983

Publisher: National Aeronautics and Space Administration, Scientific and Technical Information Branch, For sale by the National Technical Information Service]