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Aerodynamic-derivative Characteristics of the X-15 Research Airplane as Determined from Flight Tests for Mach Numbers from 0.6 to 3.4

Roxanah B. Yancey

Published: 1962

Total Pages: 72

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Aerodynamic-derivative Characteristics of the X-15 Research Airplane as Determined from Flight Tests for Mach Numbers from 0.6 to 3.4

ROXANAH B. YANCEY

Published: 1962

Total Pages: 1

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Aerodynamic-derivate Characteristics of the X-15 Research Airplane as Determined from Flight Tests for Mach Numbers from 0.6 to 3.4

Roxanah B. Yancey

Published: 1962

Total Pages: 68

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Flight Measurements of Stability and Control Derivatives of the X-15 Research Airplane to a Mach Number of 6.02 and an Angle of Attack of 250

Roxanah B. Yancey

Published: 1964

Total Pages: 56

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Scientific and Technical Aerospace Reports

Published: 1992

Total Pages: 1572

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Launch Characteristics of the X-15 Research Airplane as Determined in Flight

Gene J. Matranga

Published: 1961

Total Pages: 36

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Subject Index to Unclassified ASTIA Documents

Defense Documentation Center (U.S.)

Published: 1960

Total Pages: 306

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Keywords Index to U.S. Government Technical Reports

Published: 1962-12

Total Pages: 152

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NASA Scientific and Technical Reports

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

Published: 1967

Total Pages: 2300

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A Selected Listing of NASA Scientific and Technical Reports for 1966

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

Published: 1967

Total Pages: 2084

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Aerodynamic-derivative Characteristics of the X-15 Research Airplane as Determined from Flight Tests for Mach Numbers from 0.6 to 3.4

Aerodynamic-derivative Characteristics of the X-15 Research Airplane as Determined from Flight Tests for Mach Numbers from 0.6 to 3.4

Aerodynamic-derivate Characteristics of the X-15 Research Airplane as Determined from Flight Tests for Mach Numbers from 0.6 to 3.4

Flight Measurements of Stability and Control Derivatives of the X-15 Research Airplane to a Mach Number of 6.02 and an Angle of Attack of 250

Scientific and Technical Aerospace Reports

Launch Characteristics of the X-15 Research Airplane as Determined in Flight

Subject Index to Unclassified ASTIA Documents

Keywords Index to U.S. Government Technical Reports

NASA Scientific and Technical Reports

A Selected Listing of NASA Scientific and Technical Reports for 1966

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