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Flight-measured Aerodynamic Drag of Two Large External Tanks Attached to the X-15-2 Airplane at Mach Numbers of 1.6 to 2.3

David F. Fisher

Published: 1969

Total Pages: 22

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FLIGHT-MEASURED AERODYNAMIC DRAG OF TWO LARGE EXTERNAL TANKS ATTACHED TO THE X-15-2 AIRPLANE AT MACH NUMBERS OF 1.6 TO 2.3

UNITED STATES. NATIONAL AERONAUTICS AND SPACE ADMINISTRATION.

Published: 1965

Total Pages: 39

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NASA Scientific and Technical Reports

United States. National Aeronautics and Space Administration Scientific and Technical Information Division

Published: 1970

Total Pages: 966

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NASA Scientific and Technical Reports and Publications for 1969 - A Selected Listing

United States. National Aeronautics and Space Administration. Scientific and Technical Information Division

Published: 1970

Total Pages: 956

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A Selected Listing of NASA Scientific and Technical Reports

United States. National Aeronautics and Space Administration. Scientific and Technical Information Division

Published: 1970

Total Pages: 962

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Scientific and Technical Aerospace Reports

Published: 1983

Total Pages: 1368

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NASA SP.

Published: 1970

Total Pages: 970

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X-15 Research Results

Wendell H. Stillwell

Published: 1965

Total Pages: 140

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Comparison of Full-scale Lift and Drag Characteristics of the X-15 Airplane with Wind-tunnel Results and Theory

Edward J. Hopkins

Published: 1962

Total Pages: 22

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Preliminary Full-scale Power-off Drag of the X-15 Airplane for Mach Numbers from 0.7 to 3.1

Edwin J. Saltzman

Published: 1960

Total Pages: 28

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Books and Bottles

Flight-measured Aerodynamic Drag of Two Large External Tanks Attached to the X-15-2 Airplane at Mach Numbers of 1.6 to 2.3

FLIGHT-MEASURED AERODYNAMIC DRAG OF TWO LARGE EXTERNAL TANKS ATTACHED TO THE X-15-2 AIRPLANE AT MACH NUMBERS OF 1.6 TO 2.3

NASA Scientific and Technical Reports

NASA Scientific and Technical Reports and Publications for 1969 - A Selected Listing

A Selected Listing of NASA Scientific and Technical Reports

Scientific and Technical Aerospace Reports

NASA SP.

X-15 Research Results

Comparison of Full-scale Lift and Drag Characteristics of the X-15 Airplane with Wind-tunnel Results and Theory

Preliminary Full-scale Power-off Drag of the X-15 Airplane for Mach Numbers from 0.7 to 3.1

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