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

Stability and control characteristics of a 0.0667-scale model of the final version of the North American X-15 research airplane (configuration 3) at transonic speeds /

Osborne, Robert S.
Ware, George M.
United States. National Aeronautics and Space Administration.

"April 1963."Cover title.Includes bibliographical references (p. 8).Mode of access: Internet

Investigation of the loading characteristics of the lifting surfaces and the speed brakes of a 0.067-scale model of the north american x-15 airplane (configuration 3) at Mach numbers of 2.29, 2.98, and 4.65 /

Silvers, Norman H.
Wills, Jane S.
Lancaster, Julia A.
Langley Research Center.

January 1960

"September 1960."Cover title.Includes bibliographical references (p. 10).Mode of access: Internet

Static longitudinal, directional, and lateral stability and control data at a mach number of 6.83 of the final configuration of the X-15 research airplane /

Penland, Jim A.
Fetterman, Jr., David E.
Langley Research Center.

January 1960

"April 1960"--Cover.Caption title.Includes bibliographical references (p. 10-11).Mode of access: Int...

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

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

Operational experiences and characteristics of the X-15 flight control system /

Tremant, Robert A.
United States. National Aeronautics and Space Administration.

Cover title."December 1962."Includes bibliographical references.Mode of access: Internet

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

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

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

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

Cover title."July 1961."Aerodynamics, aircraft; Aerodynamics, missiles and space vehicles; Aircraft;...

Low-speed measurements of oscillatory lateral stability derivatives of a 1/7-scale model of the North American X-15 airplane /

Paulson, John W.
Hassell, James L.
United States. National Aeronautics and Space Administration.

"November 1959."Cover title.Includes bibliographical references (p. 6).Mode of access: Internet

Flight investigation to determine the effect of longitudinal characteristics on low-speed instrument operation /

DiCarlo, Daniel J.
Sommer, Robert W.
Kelly, James R.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."March 1968."Includes bibliographical references (p. 17).Mode of access: Internet

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

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

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

Controllability of the X-15 research airplane with interim engines during high-altitude flights /

Holleman, Euclid C.
Reisert, Donald.
United States. National Aeronautics and Space Administration.

January 1961

"March 1961."Includes bibliographical references (p. 10).Mode of access: Internet

Stability and control characteristics of a 0.0667-scale model of the final version of the North American X-15 research airplane (configuration 3) at transonic speeds /

Osborne, Robert S.
Ware, George M.
United States. National Aeronautics and Space Administration.

"April 1963."Cover title.Includes bibliographical references (p. 8).Mode of access: Internet

Investigation of the loading characteristics of the lifting surfaces and the speed brakes of a 0.067-scale model of the north american x-15 airplane (configuration 3) at Mach numbers of 2.29, 2.98, and 4.65 /

Silvers, Norman H.
Wills, Jane S.
Lancaster, Julia A.
Langley Research Center.

January 1960

"September 1960."Cover title.Includes bibliographical references (p. 10).Mode of access: Internet

Static longitudinal, directional, and lateral stability and control data at a mach number of 6.83 of the final configuration of the X-15 research airplane /

Penland, Jim A.
Fetterman, Jr., David E.
Langley Research Center.

January 1960

"April 1960"--Cover.Caption title.Includes bibliographical references (p. 10-11).Mode of access: Int...

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

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

Operational experiences and characteristics of the X-15 flight control system /

Tremant, Robert A.
United States. National Aeronautics and Space Administration.

Cover title."December 1962."Includes bibliographical references.Mode of access: Internet

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

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

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

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

Cover title."July 1961."Aerodynamics, aircraft; Aerodynamics, missiles and space vehicles; Aircraft;...

Low-speed measurements of oscillatory lateral stability derivatives of a 1/7-scale model of the North American X-15 airplane /

Paulson, John W.
Hassell, James L.
United States. National Aeronautics and Space Administration.

"November 1959."Cover title.Includes bibliographical references (p. 6).Mode of access: Internet

Flight investigation to determine the effect of longitudinal characteristics on low-speed instrument operation /

DiCarlo, Daniel J.
Sommer, Robert W.
Kelly, James R.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."March 1968."Includes bibliographical references (p. 17).Mode of access: Internet

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

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

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

Controllability of the X-15 research airplane with interim engines during high-altitude flights /

Holleman, Euclid C.
Reisert, Donald.
United States. National Aeronautics and Space Administration.

January 1961

"March 1961."Includes bibliographical references (p. 10).Mode of access: Internet

Stability and control characteristics of a 0.0667-scale model of the final version of the North American X-15 research airplane (configuration 3) at transonic speeds /

Osborne, Robert S.
Ware, George M.
United States. National Aeronautics and Space Administration.

"April 1963."Cover title.Includes bibliographical references (p. 8).Mode of access: Internet

Investigation of the loading characteristics of the lifting surfaces and the speed brakes of a 0.067-scale model of the north american x-15 airplane (configuration 3) at Mach numbers of 2.29, 2.98, and 4.65 /

Silvers, Norman H.
Wills, Jane S.
Lancaster, Julia A.
Langley Research Center.

January 1960

"September 1960."Cover title.Includes bibliographical references (p. 10).Mode of access: Internet

Static longitudinal, directional, and lateral stability and control data at a mach number of 6.83 of the final configuration of the X-15 research airplane /

Penland, Jim A.
Fetterman, Jr., David E.
Langley Research Center.

January 1960

"April 1960"--Cover.Caption title.Includes bibliographical references (p. 10-11).Mode of access: Int...

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

Abstract

Extracted data

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

Abstract

Extracted data

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