Analysis of X-15 landing approach and flare characteristics determined from the first 30 flights /

Handling qualities experience with several VTOL research aircraft /

Reeder, John P.
United States. National Aeronautics and Space Administration.

Cover title."March 1961."Aerodynamics, aircraft; Piloting; Stability and control; Vehicle performanc...

Flight investigation using variable-stability airplanes of minimum stability requirements for high-speed, high-altitude vehicles /

McFadden, Norman M.
Heinle, Donovan R.
Vomaske, Richard F.
United States. National Aeronautics and Space Administration.

Cover title."April 1961."Aerodynamics, aircraft; Aircraft; Piloting; Stability and control; Vehicle ...

Investigation of the aerodynamic characteristics of a 0.067-scale model of the x-15 airplane (configuration 3) at mach numbers of 2.29, 2.98, and 4.65 /

Franklin, Arthur E.
Lust, Robert M.
Langley Research Center.

January 1959

"November 1959."Cover title.Includes bibliographical references (p. 9).Mode of access: Internet

Aerodynamic and landing measurements obtained during the first powered flight of the North American X-15 research airplane /

United States. National Aeronautics and Space Administration.
Flight Research Center (U.S.)

"January 1960."Cover title.Includes bibliographical references (p. 17).Mode of access: Internet

Aerodynamic-derivative characteristics of the X-15 research airplane as determined from flight tests for mach numbers from 0.6 to 3.4 /

Yancey, Roxanah B.
United States. National Aeronautics and Space Administration.

Cover title."January 1962."Aerodynamics, aircraft; Aerodynamics, missiles and space vehicles; Aircra...

Preliminary base pressures obtained from the X-15 airplane at mach numbers from 1.1 to 3.2 /

Saltzman, Edwin J.
United States. National Aeronautics and Space Administration.

Cover title."August 1961."Aerodynamics, aircraft;Aerodynamics, missiles and space vehicles; Vehicle ...

Launch, low-speed, and landing characteristics determined from the first flight of the North American X-15 research airplane /

Finch, Thomas W.
Matranga, Gene J.
United States. National Aeronautics and Space Administration.

"September 1959."Cover title.Includes bibliographical references (p. 11).Mode of access: Internet

Measurement of the maximum altitude attained by the X-15 airplane powered with interim rocket engines /

Stillwell, Wendell H.
Larson, Terry J.
United States. National Aeronautics and Space Administration.

Cover title."October 1960."Aircraft; Piloting; Space vehicles; Vehicle performance.Includes bibliogr...

Landing-gear behavior during touchdown and runout for 17 landings of the X-15 research airplane /

McKay, James M.
Scott, Betty J.
United States. National Aeronautics and Space Administration.

January 1961

"March 1961."Includes bibliographical references (p. 18).Mode of access: Internet

Landing loads and dynamics of the X-15 airplane /

McKay, James M..
Kordes, Eldon E.
Flight Research Center.

January 1962

"March 1962."Includes bibliographical references (p. 11).Mode of access: Internet

Statistical analysis of landing-contact conditions for the XB-70 airplane /

Wilson, Ronald J.
Larson, Richard R.
Flight Research Center (U.S.)
United States. National Aeronautics and Space Administration.

January 1967

Cover title."June 1967."Includes bibliographical references (p. 11).Mode of access: Internet

Review of the X-15 program Joseph Weil.

Weil, Joseph.
United States. National Aeronautics and Space Administration.

Cover title."June 1962."Aerodynamics, aircraft; Aircraft; Biomedicine; Piloting; Propulsion systems,...

Handling qualities of the XB-70 airplane in the landing approach.

Berry, Donald T.
Powers, Bruce G.
Flight Research Center.
United States. National Aeronautics and Space Administration.

Approach and landing performance of XB-70 aircraft.Prepared at Flight Research Center."February 1970...

Approach and landing investigation at lift-drag ratios of 2 to 4 utilizing a straight-wing fighter airplane /

Matranga, Gene J.
Armstrong, Neil, 1930-
United States. National Aeronautics and Space Administration.

"August 1959."Cover title.Includes bibliographical references (p. 10).Mode of access: Internet

Preliminary results of aerodynamic heating studies on the X-15 airplane /

Banner, Richard D.
Quinn, Robert D.
Kuhl, Albert E.
Flight Research Center (U.S.)

January 1962

"March 1962."Cover title.Includes bibliographical references (p. 12).Mode of access: Internet

Handling qualities experience with several VTOL research aircraft /

Reeder, John P.
United States. National Aeronautics and Space Administration.

Cover title."March 1961."Aerodynamics, aircraft; Piloting; Stability and control; Vehicle performanc...

Flight investigation using variable-stability airplanes of minimum stability requirements for high-speed, high-altitude vehicles /

McFadden, Norman M.
Heinle, Donovan R.
Vomaske, Richard F.
United States. National Aeronautics and Space Administration.

Cover title."April 1961."Aerodynamics, aircraft; Aircraft; Piloting; Stability and control; Vehicle ...

Investigation of the aerodynamic characteristics of a 0.067-scale model of the x-15 airplane (configuration 3) at mach numbers of 2.29, 2.98, and 4.65 /

Franklin, Arthur E.
Lust, Robert M.
Langley Research Center.

January 1959

"November 1959."Cover title.Includes bibliographical references (p. 9).Mode of access: Internet

Aerodynamic and landing measurements obtained during the first powered flight of the North American X-15 research airplane /

United States. National Aeronautics and Space Administration.
Flight Research Center (U.S.)

"January 1960."Cover title.Includes bibliographical references (p. 17).Mode of access: Internet

Aerodynamic-derivative characteristics of the X-15 research airplane as determined from flight tests for mach numbers from 0.6 to 3.4 /

Yancey, Roxanah B.
United States. National Aeronautics and Space Administration.

Cover title."January 1962."Aerodynamics, aircraft; Aerodynamics, missiles and space vehicles; Aircra...

Preliminary base pressures obtained from the X-15 airplane at mach numbers from 1.1 to 3.2 /

Saltzman, Edwin J.
United States. National Aeronautics and Space Administration.

Cover title."August 1961."Aerodynamics, aircraft;Aerodynamics, missiles and space vehicles; Vehicle ...

Launch, low-speed, and landing characteristics determined from the first flight of the North American X-15 research airplane /

Finch, Thomas W.
Matranga, Gene J.
United States. National Aeronautics and Space Administration.

"September 1959."Cover title.Includes bibliographical references (p. 11).Mode of access: Internet

Measurement of the maximum altitude attained by the X-15 airplane powered with interim rocket engines /

Stillwell, Wendell H.
Larson, Terry J.
United States. National Aeronautics and Space Administration.

Cover title."October 1960."Aircraft; Piloting; Space vehicles; Vehicle performance.Includes bibliogr...

Landing-gear behavior during touchdown and runout for 17 landings of the X-15 research airplane /

McKay, James M.
Scott, Betty J.
United States. National Aeronautics and Space Administration.

January 1961

"March 1961."Includes bibliographical references (p. 18).Mode of access: Internet

Landing loads and dynamics of the X-15 airplane /

McKay, James M..
Kordes, Eldon E.
Flight Research Center.

January 1962

"March 1962."Includes bibliographical references (p. 11).Mode of access: Internet

Statistical analysis of landing-contact conditions for the XB-70 airplane /

Wilson, Ronald J.
Larson, Richard R.
Flight Research Center (U.S.)
United States. National Aeronautics and Space Administration.

January 1967

Cover title."June 1967."Includes bibliographical references (p. 11).Mode of access: Internet

Review of the X-15 program Joseph Weil.

Weil, Joseph.
United States. National Aeronautics and Space Administration.

Cover title."June 1962."Aerodynamics, aircraft; Aircraft; Biomedicine; Piloting; Propulsion systems,...

Handling qualities of the XB-70 airplane in the landing approach.

Berry, Donald T.
Powers, Bruce G.
Flight Research Center.
United States. National Aeronautics and Space Administration.

Approach and landing performance of XB-70 aircraft.Prepared at Flight Research Center."February 1970...

Approach and landing investigation at lift-drag ratios of 2 to 4 utilizing a straight-wing fighter airplane /

Matranga, Gene J.
Armstrong, Neil, 1930-
United States. National Aeronautics and Space Administration.

"August 1959."Cover title.Includes bibliographical references (p. 10).Mode of access: Internet

Preliminary results of aerodynamic heating studies on the X-15 airplane /

Banner, Richard D.
Quinn, Robert D.
Kuhl, Albert E.
Flight Research Center (U.S.)

January 1962

"March 1962."Cover title.Includes bibliographical references (p. 12).Mode of access: Internet

Handling qualities experience with several VTOL research aircraft /

Reeder, John P.
United States. National Aeronautics and Space Administration.

Cover title."March 1961."Aerodynamics, aircraft; Piloting; Stability and control; Vehicle performanc...

Flight investigation using variable-stability airplanes of minimum stability requirements for high-speed, high-altitude vehicles /

McFadden, Norman M.
Heinle, Donovan R.
Vomaske, Richard F.
United States. National Aeronautics and Space Administration.

Cover title."April 1961."Aerodynamics, aircraft; Aircraft; Piloting; Stability and control; Vehicle ...

Investigation of the aerodynamic characteristics of a 0.067-scale model of the x-15 airplane (configuration 3) at mach numbers of 2.29, 2.98, and 4.65 /

Franklin, Arthur E.
Lust, Robert M.
Langley Research Center.

January 1959

"November 1959."Cover title.Includes bibliographical references (p. 9).Mode of access: Internet

Analysis of X-15 landing approach and flare characteristics determined from the first 30 flights /

Abstract

Extracted data

Analysis of X-15 landing approach and flare characteristics determined from the first 30 flights /

Abstract

Extracted data

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