The use of drag modulation to limit the rate at which deceleration increases during nonlifting entry /

Some effects of leading-edge sweep on boundary-layer transition at supersonic speeds /

Chapman, Gary T.
United States. National Aeronautics and Space Administration.

Cover title."September 1961."Aerodynamics, aircraft; Aerodynamics, missiles and space vehicles; Flui...

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...

Drag characteristics and dynamic stability in descent of a rotary parachute tested in a vertical tunnel /

Burk, Sanger M.
United States. National Aeronautics and Space Administration.

Cover title."August 1962."Aerodynamics, missiles and space vehicles; Atmospheric entry.Includes bibl...

Atmosphere entries with vehicle lift-drag ration modulated to limit deceleration and rate of deceleration: vehicles with maximum lift-drag ration of 0.5 /

Katzen, Elliott D.
Levy, Lionel L.
United States. National Aeronautics and Space Administration.

Cover title."December 1961."Aerodynamics, missiles and space vehicles; Atmospheric entry.Includes bi...

Atmosphere entries with spacecraft lift-drag ratios modulated to limit decelerations / Lionel L. Levy Jr.

Levy, Lionel L.
United States. National Aeronautics and Space Administration.

Cover title."October 1962."Aerodynamics, missiles and space vehicles; Atmospheric entry; Space mecha...

Importance of the variation of drag with lift in minimization of satellite entry acceleration /

Grant, Frederick C.
Langley Research Center.

January 1959

"NASA TN D-120.""Langley Research Center, Langley Field, Va.""October 1959."Title from cover.Include...

An approximate analytical method for studying atmosphere entry of vehicles with modulated aerodynamic forces /

Levy, Lionel L.
United States. National Aeronautics and Space Administration.

Cover title."October 1960."Aerodynamics, missiles and space vehicles; Atmospheric entry.Includes bib...

Aerodynamic characteristics of towed cones used as decelerators at mach numbers rom 1.57 to 4.65 /

Charczenko, Nickolai.
McShera, John T.
United States. National Aeronautics and Space Administration.

Cover title." December 1961."Aerodynamics, missiles and space vehicles;Atmospheric entry.Includes bi...

A note on the drag due to lift of delta wings at mach numbers up to 2.0 /

Osborne, Robert S.
Kelly, Thomas C.
United States. National Aeronautics and Space Administration.

Cover title."November 1960."Aerodynamics, aircraft; Aircraft.Includes bibliographical references.Mod...

Investigation of a retrorocket exhausting from the nose of a blunt body into a supersonic free stream /

Charczenko, Nickolai.
Hennessey, Katherine W.
United States. National Aeronautics and Space Administration.

Cover title."September 1961."Aerodynamics, missiles and space vehicles; Atmospheric entry.Includes b...

The effect of thrust minus base drag of exchanging base area for nozzle expansion in supersonic nozzles at transonic mach numbers /

Slocumb, Travis H.
Andrews, Earl H.
United States. National Aeronautics and Space Administration.

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

Aerodynamic drag and stability characteristics of towed inflatable decelerations at supersonic speeds

McShera, John T.
United States. National Aeronautics and Space Administration.

Cover title."March 1963."Includes bibliographical references.Mode of access: Internet

Effects of cone angel, mach number, and nose blunting on transition at supersonic speeds /

Czarnecki, K. R.
United States. National Aeronautics and Space Administration.

Cover title."November 1960."Aerodynamics, aircraft; Aerodynamics, missiles and space vehicles; Fluid...

Axial-force reduction by interference between jet and neighboring afterbody /

Pitts, William C.
Wiggins, Lyle E.
United States. National Aeronautics and Space Administration.

Cover title."September 1960."Aerodynamics, missiles and space vehicles.Includes bibliographical refe...

A preliminary study of the use of finite-thrust engines for abort during launch of space vehicles /

McGowan, William A.
United States. National Aeronautics and Space Administration.

Cover title."December 1961."Atmospheric entry; Space mechanics; Space vehicles.Includes bibliographi...

Some effects of leading-edge sweep on boundary-layer transition at supersonic speeds /

Chapman, Gary T.
United States. National Aeronautics and Space Administration.

Cover title."September 1961."Aerodynamics, aircraft; Aerodynamics, missiles and space vehicles; Flui...

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...

Drag characteristics and dynamic stability in descent of a rotary parachute tested in a vertical tunnel /

Burk, Sanger M.
United States. National Aeronautics and Space Administration.

Cover title."August 1962."Aerodynamics, missiles and space vehicles; Atmospheric entry.Includes bibl...

Atmosphere entries with vehicle lift-drag ration modulated to limit deceleration and rate of deceleration: vehicles with maximum lift-drag ration of 0.5 /

Katzen, Elliott D.
Levy, Lionel L.
United States. National Aeronautics and Space Administration.

Cover title."December 1961."Aerodynamics, missiles and space vehicles; Atmospheric entry.Includes bi...

Atmosphere entries with spacecraft lift-drag ratios modulated to limit decelerations / Lionel L. Levy Jr.

Levy, Lionel L.
United States. National Aeronautics and Space Administration.

Cover title."October 1962."Aerodynamics, missiles and space vehicles; Atmospheric entry; Space mecha...

Importance of the variation of drag with lift in minimization of satellite entry acceleration /

Grant, Frederick C.
Langley Research Center.

January 1959

"NASA TN D-120.""Langley Research Center, Langley Field, Va.""October 1959."Title from cover.Include...

An approximate analytical method for studying atmosphere entry of vehicles with modulated aerodynamic forces /

Levy, Lionel L.
United States. National Aeronautics and Space Administration.

Cover title."October 1960."Aerodynamics, missiles and space vehicles; Atmospheric entry.Includes bib...

Aerodynamic characteristics of towed cones used as decelerators at mach numbers rom 1.57 to 4.65 /

Charczenko, Nickolai.
McShera, John T.
United States. National Aeronautics and Space Administration.

Cover title." December 1961."Aerodynamics, missiles and space vehicles;Atmospheric entry.Includes bi...

A note on the drag due to lift of delta wings at mach numbers up to 2.0 /

Osborne, Robert S.
Kelly, Thomas C.
United States. National Aeronautics and Space Administration.

Cover title."November 1960."Aerodynamics, aircraft; Aircraft.Includes bibliographical references.Mod...

Investigation of a retrorocket exhausting from the nose of a blunt body into a supersonic free stream /

Charczenko, Nickolai.
Hennessey, Katherine W.
United States. National Aeronautics and Space Administration.

Cover title."September 1961."Aerodynamics, missiles and space vehicles; Atmospheric entry.Includes b...

The effect of thrust minus base drag of exchanging base area for nozzle expansion in supersonic nozzles at transonic mach numbers /

Slocumb, Travis H.
Andrews, Earl H.
United States. National Aeronautics and Space Administration.

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

Aerodynamic drag and stability characteristics of towed inflatable decelerations at supersonic speeds

McShera, John T.
United States. National Aeronautics and Space Administration.

Cover title."March 1963."Includes bibliographical references.Mode of access: Internet

Effects of cone angel, mach number, and nose blunting on transition at supersonic speeds /

Czarnecki, K. R.
United States. National Aeronautics and Space Administration.

Cover title."November 1960."Aerodynamics, aircraft; Aerodynamics, missiles and space vehicles; Fluid...

Axial-force reduction by interference between jet and neighboring afterbody /

Pitts, William C.
Wiggins, Lyle E.
United States. National Aeronautics and Space Administration.

Cover title."September 1960."Aerodynamics, missiles and space vehicles.Includes bibliographical refe...

A preliminary study of the use of finite-thrust engines for abort during launch of space vehicles /

McGowan, William A.
United States. National Aeronautics and Space Administration.

Cover title."December 1961."Atmospheric entry; Space mechanics; Space vehicles.Includes bibliographi...

Some effects of leading-edge sweep on boundary-layer transition at supersonic speeds /

Chapman, Gary T.
United States. National Aeronautics and Space Administration.

Cover title."September 1961."Aerodynamics, aircraft; Aerodynamics, missiles and space vehicles; Flui...

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...

Drag characteristics and dynamic stability in descent of a rotary parachute tested in a vertical tunnel /

Burk, Sanger M.
United States. National Aeronautics and Space Administration.

Cover title."August 1962."Aerodynamics, missiles and space vehicles; Atmospheric entry.Includes bibl...

The use of drag modulation to limit the rate at which deceleration increases during nonlifting entry /

Abstract

Extracted data

The use of drag modulation to limit the rate at which deceleration increases during nonlifting entry /

Abstract

Extracted data

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