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

Investigation of the subsonic stability and control characteristics of a 1/7-scale model of the North American X-15 airplane with and without fuselage forebody strakes /

Hassell, James L.
Hewes, Donald E.
United States. National Aeronautics and Space Administration.

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

Characteristics and use of X-15 air-data sensors /

Webb, Lannie D.
Flight Research Center (U.S.)
United States. National Aeronautics and Space Administration.

January 1968

Cover title."June 1968."Includes bibliographical references (p. 26-28).Mode of access: Internet

Precision controllability of the F-15 airplane,

Sisk, Thomas R.
Matheny, Neil W.
Hugh L. Dryden Flight Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1979

"May 1979"--Cover."Dryden Flight Research Center, Edwards, California."Includes bibliographical refe...

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

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...

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

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

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

Transonic flutter investigation of models of the X-15 airplane horizontal tail /

Young, Lou S.
Bland, Samuel R.
Langley Research Center.

January 1961

"February 1961."Caption title.Includes bibliographical references (p. 14).Mode of access: Internet

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

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

Preliminary flight evaluation of the stability and control derivatives and dynamic characteristics of the unaugmented XB-70-1 airplane including comparisons with predictions /

Wolowicz, Chester H.
Flight Research Center (U.S.)
United States. National Aeronautics and Space Administration.

January 1968

Cover title."May 1968."Includes bibliographical references (p. 25).Mode of access: Internet

Flight Behavior of the X-2 research airplane to a Mach number of 3.20 and a geometric altitude of 126,200 feet /

Day, Richard E.
Reisert, Donald.
High-Speed Flight Station. Edwards, Calif.

January 1959

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

Investigation of the subsonic stability and control characteristics of a 1/7-scale model of the North American X-15 airplane with and without fuselage forebody strakes /

Hassell, James L.
Hewes, Donald E.
United States. National Aeronautics and Space Administration.

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

Characteristics and use of X-15 air-data sensors /

Webb, Lannie D.
Flight Research Center (U.S.)
United States. National Aeronautics and Space Administration.

January 1968

Cover title."June 1968."Includes bibliographical references (p. 26-28).Mode of access: Internet

Precision controllability of the F-15 airplane,

Sisk, Thomas R.
Matheny, Neil W.
Hugh L. Dryden Flight Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1979

"May 1979"--Cover."Dryden Flight Research Center, Edwards, California."Includes bibliographical refe...

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

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...

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

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

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

Transonic flutter investigation of models of the X-15 airplane horizontal tail /

Young, Lou S.
Bland, Samuel R.
Langley Research Center.

January 1961

"February 1961."Caption title.Includes bibliographical references (p. 14).Mode of access: Internet

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

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

Preliminary flight evaluation of the stability and control derivatives and dynamic characteristics of the unaugmented XB-70-1 airplane including comparisons with predictions /

Wolowicz, Chester H.
Flight Research Center (U.S.)
United States. National Aeronautics and Space Administration.

January 1968

Cover title."May 1968."Includes bibliographical references (p. 25).Mode of access: Internet

Flight Behavior of the X-2 research airplane to a Mach number of 3.20 and a geometric altitude of 126,200 feet /

Day, Richard E.
Reisert, Donald.
High-Speed Flight Station. Edwards, Calif.

January 1959

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

Investigation of the subsonic stability and control characteristics of a 1/7-scale model of the North American X-15 airplane with and without fuselage forebody strakes /

Hassell, James L.
Hewes, Donald E.
United States. National Aeronautics and Space Administration.

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

Characteristics and use of X-15 air-data sensors /

Webb, Lannie D.
Flight Research Center (U.S.)
United States. National Aeronautics and Space Administration.

January 1968

Cover title."June 1968."Includes bibliographical references (p. 26-28).Mode of access: Internet

Precision controllability of the F-15 airplane,

Sisk, Thomas R.
Matheny, Neil W.
Hugh L. Dryden Flight Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1979

"May 1979"--Cover."Dryden Flight Research Center, Edwards, California."Includes bibliographical refe...

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

Abstract

Extracted data

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

Abstract

Extracted data

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