Static longitudinal and lateral stability characteristics at a mach number of 3.11 of square and circular plan-form reentry vehicles, with some effects of controls and leading-edge extensions /

Longitudinal and lateral stability characteristics of two four-jet vtol models in the transition speed range /

Vogler, Raymond D.
Kuhn, Richard E.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1965

"May 1965."Cover title.Includes bibliographical references (p. 17).Mode of access: Internet

Investigation of the low-subsonic stability and control characteristics of a 0.34-scale free-flying model of a modified half-cone reentry vehicle /

Hassell, James L.
Ware, George M.
United States. National Aeronautics and Space Administration.

"January 1962."Cover title.Includes bibliographical references (p. 15).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...

Low-subsonic-speed static longitudinal stability and control characteristics of a winged reentry-vehicle configuration having wingtip panels that fold up for high-drag reentry /

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

"February 1960."Cover title.Includes bibliographical references (p. 5).Mode of access: Internet

Static longitudinal aerodynamic characteristics at transonic speeds of a lenticular-shaped reentry vehicle /

Mugler, John P.
Olstad, Walter B.
United States. National Aeronautics and Space Administration.

"December 1960."Cover title.Includes bibliographical references (p. 11).Mode of access: Internet

Static longitudinal aerodynamic characteristics at a Mach number of 10.03 of low-aspect-ratio wing-body configurations suitable for reentry /

Putnam, Lawrence E. (Lawrence Elwood)
Brooks, Cuyler W.
Langley Research Center.

January 1962

"December 1962."Cover title.Includes bibliographical references (p. 9).Mode of access: Internet

Exploratory investigation at mach number of 2.01 of the longitudinal stability and control characteristics of a winged reentry configuration /

Foster, Gerald V.
United States. National Aeronautics and Space Administration.

"December 1959."Cover title.Includes bibliographical references (p. 7).Mode of access: Internet

Low-subsonic-speed static stability of right-triangular-pyramid and half-cone lifting reentry configurations. /

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

Abstract:Cover title."February 1961."Aerodynamics, missiles and space vehicles; Space vehicles; Stab...

Static longitudinal stability characteristics of a blunted glider reentry configuration having 79.5° sweepback and 45° dihedral at mach number of 6.2 and angles of attack up to 20° /

Mayo, Edward E.
United States. National Aeronautics and Space Administration.

"October 1959."Cover title.Includes bibliographical references (p. 7).Mode of access: Internet

The lateral and directional aerodynamic characteristics of a re-entry configuration based on a blunt 13° half cone at Mach numbers to 0.90 /

Kenyon, George C.
Ames Research Center.

January 1961

"November 1961."Cover title.Includes bibliographical references (p. 10).Mode of access: Internet

Static longitudinal stability and control characteristics at a mach number of 2.01 of a hypersonic missile configuration having all-movable wing and tail surfaces /

Robinson, Ross B.
Foster, Gerald V.
Langley Research Center.

January 1961

"April 1961."Cover title.Includes bibliographical references (p. 6).Mode of access: Internet

Aerodynamic characteristics of three axismmetric low-fitness-ratio reentry shapes at Mach 6.9 /

Penland, Jim A.
Bernot, Peter T.
United States. National Aeronautics and Space Administration.

January 1967

Cover title."August 1967."Includes bibliographical references (p. 10).Mode of access: Internet

Wind-tunnel investigation at high subsonic speed of the static longitudinal stability characteristics of a winged reentry vehicle having a large negatively deflected flap-type control surface /

Fournier, Paul G.
United States. National Aeronautics and Space Administration.

"December 1959."Cover title.Includes bibliographical references (p. 7).Mode of access: Internet

Effect of longitudinal and lateral controls on winged reentry configuration at mach 1.97 and angles of attack up to 90° /

Foster, Gerald V.
United States. National Aeronautics and Space Administration.

January 1961

"February 1961."Includes bibliographical references (p. 5).Mode of access: Internet

Static longitudinal stability characteristics of various Mercury escape configurations and of a proposed alternate escape configuration for Mach numbers of 0.05 to 9.60 /

Smith, Robert P.
Moseley, William C.
United States. National Aeronautics and Space Administration. Space Task Group.

January 1961

"July 1961."Cover title.Includes bibliographical references (p. 16-17).Mode of access: Internet

Longitudinal and lateral stability characteristics of two four-jet vtol models in the transition speed range /

Vogler, Raymond D.
Kuhn, Richard E.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1965

"May 1965."Cover title.Includes bibliographical references (p. 17).Mode of access: Internet

Investigation of the low-subsonic stability and control characteristics of a 0.34-scale free-flying model of a modified half-cone reentry vehicle /

Hassell, James L.
Ware, George M.
United States. National Aeronautics and Space Administration.

"January 1962."Cover title.Includes bibliographical references (p. 15).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...

Low-subsonic-speed static longitudinal stability and control characteristics of a winged reentry-vehicle configuration having wingtip panels that fold up for high-drag reentry /

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

"February 1960."Cover title.Includes bibliographical references (p. 5).Mode of access: Internet

Static longitudinal aerodynamic characteristics at transonic speeds of a lenticular-shaped reentry vehicle /

Mugler, John P.
Olstad, Walter B.
United States. National Aeronautics and Space Administration.

"December 1960."Cover title.Includes bibliographical references (p. 11).Mode of access: Internet

Static longitudinal aerodynamic characteristics at a Mach number of 10.03 of low-aspect-ratio wing-body configurations suitable for reentry /

Putnam, Lawrence E. (Lawrence Elwood)
Brooks, Cuyler W.
Langley Research Center.

January 1962

"December 1962."Cover title.Includes bibliographical references (p. 9).Mode of access: Internet

Exploratory investigation at mach number of 2.01 of the longitudinal stability and control characteristics of a winged reentry configuration /

Foster, Gerald V.
United States. National Aeronautics and Space Administration.

"December 1959."Cover title.Includes bibliographical references (p. 7).Mode of access: Internet

Low-subsonic-speed static stability of right-triangular-pyramid and half-cone lifting reentry configurations. /

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

Abstract:Cover title."February 1961."Aerodynamics, missiles and space vehicles; Space vehicles; Stab...

Static longitudinal stability characteristics of a blunted glider reentry configuration having 79.5° sweepback and 45° dihedral at mach number of 6.2 and angles of attack up to 20° /

Mayo, Edward E.
United States. National Aeronautics and Space Administration.

"October 1959."Cover title.Includes bibliographical references (p. 7).Mode of access: Internet

The lateral and directional aerodynamic characteristics of a re-entry configuration based on a blunt 13° half cone at Mach numbers to 0.90 /

Kenyon, George C.
Ames Research Center.

January 1961

"November 1961."Cover title.Includes bibliographical references (p. 10).Mode of access: Internet

Static longitudinal stability and control characteristics at a mach number of 2.01 of a hypersonic missile configuration having all-movable wing and tail surfaces /

Robinson, Ross B.
Foster, Gerald V.
Langley Research Center.

January 1961

"April 1961."Cover title.Includes bibliographical references (p. 6).Mode of access: Internet

Aerodynamic characteristics of three axismmetric low-fitness-ratio reentry shapes at Mach 6.9 /

Penland, Jim A.
Bernot, Peter T.
United States. National Aeronautics and Space Administration.

January 1967

Cover title."August 1967."Includes bibliographical references (p. 10).Mode of access: Internet

Wind-tunnel investigation at high subsonic speed of the static longitudinal stability characteristics of a winged reentry vehicle having a large negatively deflected flap-type control surface /

Fournier, Paul G.
United States. National Aeronautics and Space Administration.

"December 1959."Cover title.Includes bibliographical references (p. 7).Mode of access: Internet

Effect of longitudinal and lateral controls on winged reentry configuration at mach 1.97 and angles of attack up to 90° /

Foster, Gerald V.
United States. National Aeronautics and Space Administration.

January 1961

"February 1961."Includes bibliographical references (p. 5).Mode of access: Internet

Static longitudinal stability characteristics of various Mercury escape configurations and of a proposed alternate escape configuration for Mach numbers of 0.05 to 9.60 /

Smith, Robert P.
Moseley, William C.
United States. National Aeronautics and Space Administration. Space Task Group.

January 1961

"July 1961."Cover title.Includes bibliographical references (p. 16-17).Mode of access: Internet

Longitudinal and lateral stability characteristics of two four-jet vtol models in the transition speed range /

Vogler, Raymond D.
Kuhn, Richard E.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1965

"May 1965."Cover title.Includes bibliographical references (p. 17).Mode of access: Internet

Investigation of the low-subsonic stability and control characteristics of a 0.34-scale free-flying model of a modified half-cone reentry vehicle /

Hassell, James L.
Ware, George M.
United States. National Aeronautics and Space Administration.

"January 1962."Cover title.Includes bibliographical references (p. 15).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...

Static longitudinal and lateral stability characteristics at a mach number of 3.11 of square and circular plan-form reentry vehicles, with some effects of controls and leading-edge extensions /

Abstract

Extracted data

Static longitudinal and lateral stability characteristics at a mach number of 3.11 of square and circular plan-form reentry vehicles, with some effects of controls and leading-edge extensions /

Abstract

Extracted data

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