Investigation of the low-subsonic aerodynamic characteristics of a model of a modified lenticular reentry configuration /

A preliminary investigation of modified blunt 13° half-cone re-entry configurations at subsonic speeds /

Kenyon, George C.
Edwards, George G.
Ames Research Center.

January 1961

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

Model investigation of the landing characteristics of a reentry spacecraft with a vertical-cylinder air bag for load alleviation /

McGehee, John R.
Vaughan, Victor L.
United States. National Aeronautics and Space Administration.

Cover title."March 1962."Aerodynamics, missiles and space vehicles; Space vehicles.Includes bibliogr...

Subsonic aerodynamic characteristics of disk re-entry configurations with elliptic cross sections and thickness-diameter ratios of 0.225 and 0.325 /

Demele, Fred A.
Brownson, Jack J.
United States. National Aeronautics and Space Administration.

"May 1961."Cover title.Includes bibliographical references (p. 9-10).Mode of access: Internet

Investigation of the low-subsonic flight characteristics of a model of a reentry vehicle with a thick flat 75 degree swept delta wing and a half-cone fuselage /

Boisseau, Peter C.
United States. National Aeronautics and Space Administration.

Cover title."February 1962."Aerodynamics, aircraft; Aerodynamics, missiles and space vehicles; Satel...

Investigation of the low-subsonic stability and control characteristics of a 1/3-scale free-flying model of a lifting-body reentry configuration /

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

"July 1960."Cover title.Includes bibliographical references (p. 14).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

Experimental investigation of a disk-shaped reentry configuration at transonic and low supersonic speeds /

Lazzeroni, Frank A.
United States. National Aeronautics and Space Administration.

"May 1962."Cover title.Includes bibliographical references (p. 7).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

Investigation of low-subsonic flight characteristics of a model of a hypersonic boost-glide configuration having a 78 degree delta wing /by /

Paulson, John W.
Shanks, Robert E.
United States. National Aeronautics and Space Administration.

January 1959

Cover title."October 1959."Includes bibliographical references.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

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 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

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

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...

A preliminary investigation of modified blunt 13° half-cone re-entry configurations at subsonic speeds /

Kenyon, George C.
Edwards, George G.
Ames Research Center.

January 1961

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

Model investigation of the landing characteristics of a reentry spacecraft with a vertical-cylinder air bag for load alleviation /

McGehee, John R.
Vaughan, Victor L.
United States. National Aeronautics and Space Administration.

Cover title."March 1962."Aerodynamics, missiles and space vehicles; Space vehicles.Includes bibliogr...

Subsonic aerodynamic characteristics of disk re-entry configurations with elliptic cross sections and thickness-diameter ratios of 0.225 and 0.325 /

Demele, Fred A.
Brownson, Jack J.
United States. National Aeronautics and Space Administration.

"May 1961."Cover title.Includes bibliographical references (p. 9-10).Mode of access: Internet

Investigation of the low-subsonic flight characteristics of a model of a reentry vehicle with a thick flat 75 degree swept delta wing and a half-cone fuselage /

Boisseau, Peter C.
United States. National Aeronautics and Space Administration.

Cover title."February 1962."Aerodynamics, aircraft; Aerodynamics, missiles and space vehicles; Satel...

Investigation of the low-subsonic stability and control characteristics of a 1/3-scale free-flying model of a lifting-body reentry configuration /

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

"July 1960."Cover title.Includes bibliographical references (p. 14).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

Experimental investigation of a disk-shaped reentry configuration at transonic and low supersonic speeds /

Lazzeroni, Frank A.
United States. National Aeronautics and Space Administration.

"May 1962."Cover title.Includes bibliographical references (p. 7).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

Investigation of low-subsonic flight characteristics of a model of a hypersonic boost-glide configuration having a 78 degree delta wing /by /

Paulson, John W.
Shanks, Robert E.
United States. National Aeronautics and Space Administration.

January 1959

Cover title."October 1959."Includes bibliographical references.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

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 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

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

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...

A preliminary investigation of modified blunt 13° half-cone re-entry configurations at subsonic speeds /

Kenyon, George C.
Edwards, George G.
Ames Research Center.

January 1961

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

Model investigation of the landing characteristics of a reentry spacecraft with a vertical-cylinder air bag for load alleviation /

McGehee, John R.
Vaughan, Victor L.
United States. National Aeronautics and Space Administration.

Cover title."March 1962."Aerodynamics, missiles and space vehicles; Space vehicles.Includes bibliogr...

Subsonic aerodynamic characteristics of disk re-entry configurations with elliptic cross sections and thickness-diameter ratios of 0.225 and 0.325 /

Demele, Fred A.
Brownson, Jack J.
United States. National Aeronautics and Space Administration.

"May 1961."Cover title.Includes bibliographical references (p. 9-10).Mode of access: Internet

Investigation of the low-subsonic aerodynamic characteristics of a model of a modified lenticular reentry configuration /

Abstract

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Investigation of the low-subsonic aerodynamic characteristics of a model of a modified lenticular reentry configuration /

Abstract

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