Theoretical investigation of effects of changes in command computations and filter location on response of an automatically controlled interceptor during the attack phase /

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...

Preliminary studies of manned satellites wingless configuration : nonlifting /

Faget, Maxime A. (Maxime Allan), 1921-2004.
Buglia, James J.
Garland, Benjamine J.
United States. National Aeronautics and Space Administration.

Cover title."March 1962."Aerodynamics, missiles and space vehicles; Atmospheric entry.Includes bibli...

Numerical analysis of the transient responce of advanced thermal protection systems for atmosphereic entry / Robert T. Swann and Claud M. Pittman.

Swann, Robert T.
Pittman, C. M. (Claud M.)
United States. National Aeronautics and Space Administration.

Cover title."July 1962."Aerodynamics, missiles and space vehicles; Atmospheric entry; Fluid mechanic...

Theoretical analysis of the longitudinal behavior of an automatically controlled supersonic interceptor during the attack phase [electronic resource] /

Gates, Ordway B.
United States. National Aeronautics and Space Administration.

January 1959

"1959."Includes bibliographical references.Mode of access: Internet.System requirement: Adobe Acroba...

Exploratory tests of the effects of jet plumes on the flow over cone-cylinder-flare bodies /

Falanga, Ralph A.
Crawford, Davis H.
Hinson, William F.
United States. National Aeronautics and Space Administration.

Cover title."February 1962."Aerodynamics, missiles and space vehicles.Includes bibliographical refer...

An exploratory investigation of jet-blast effects on a dust-covered surface at low ambient pressure /

Spady, Amos A.
United States. National Aeronautics and Space Administration.

Cover title."February 1962."Aerodynamics, missiles and space vehicles; Fluid mechanics; Space vehicl...

A study of the optimum velocity change to intercept and rendezvous /

Eggleston, John M.
United States. National Aeronautics and Space Administration.

Cover title."February 1962."Guidance and homing systems; Space mechanics; Satellites.Includes biblio...

The effect of various missile characteristics on airframe frequency response /

Matthews, Howard F.
McNeill, Walter E., joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Ames Research Center.

On front cover: "January 7, 1952, Declassified December 13, 1957."Includes bibliographical reference...

Effects of flight conditions at booster separation on payload weight in orbit /

Nelson, Richard D.
United States. National Aeronautics and Space Administration.

Cover title."November 1961."Missiles and satellite carriers; Space mechanics.Includes bibliographica...

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...

Investigation toward simplification of missile control systems /

Curfman, Howard J.
Crane, Harold L.
Strass, H. Kurt.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.
United States. National Advisory Committee for Aeronautics.

January 1953

"November 12, 1953."Includes bibliographical references (p. 7).Mode of access: Internet

Predicted shock envelopes about two types of vehicles at large angles of attack /

Kaattari, George E.
United States. National Aeronautics and Space Administration.

Cover title."April 1961."Aerodynamics, missiles and space vehicles; Fluid mechanics.Includes bibliog...

A study of a pilots ability to control during simulated stability augmentation system failures

Sadoff, Melvin.
United States. National Aeronautics and Space Administration.

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

Comparison of two maneuvers for longitudinal range control during atmospheric entry /

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

Cover title."Januery 1962."Aerodynamics, missiles and space vehicles; Atmospheric entry.Includes bib...

A theoretical investigation of the effect of cross-control derivatives on the stability characteristics of airplanes designed for flight at high mach numbers /

Brown, Lawrence W.
United States. National Aeronautics and Space Administration.

Cover title."March 1962."Aerodynamics, aircraft; Stability and control.Includes bibliographical refe...

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...

Preliminary studies of manned satellites wingless configuration : nonlifting /

Faget, Maxime A. (Maxime Allan), 1921-2004.
Buglia, James J.
Garland, Benjamine J.
United States. National Aeronautics and Space Administration.

Cover title."March 1962."Aerodynamics, missiles and space vehicles; Atmospheric entry.Includes bibli...

Numerical analysis of the transient responce of advanced thermal protection systems for atmosphereic entry / Robert T. Swann and Claud M. Pittman.

Swann, Robert T.
Pittman, C. M. (Claud M.)
United States. National Aeronautics and Space Administration.

Cover title."July 1962."Aerodynamics, missiles and space vehicles; Atmospheric entry; Fluid mechanic...

Theoretical analysis of the longitudinal behavior of an automatically controlled supersonic interceptor during the attack phase [electronic resource] /

Gates, Ordway B.
United States. National Aeronautics and Space Administration.

January 1959

"1959."Includes bibliographical references.Mode of access: Internet.System requirement: Adobe Acroba...

Exploratory tests of the effects of jet plumes on the flow over cone-cylinder-flare bodies /

Falanga, Ralph A.
Crawford, Davis H.
Hinson, William F.
United States. National Aeronautics and Space Administration.

Cover title."February 1962."Aerodynamics, missiles and space vehicles.Includes bibliographical refer...

An exploratory investigation of jet-blast effects on a dust-covered surface at low ambient pressure /

Spady, Amos A.
United States. National Aeronautics and Space Administration.

Cover title."February 1962."Aerodynamics, missiles and space vehicles; Fluid mechanics; Space vehicl...

A study of the optimum velocity change to intercept and rendezvous /

Eggleston, John M.
United States. National Aeronautics and Space Administration.

Cover title."February 1962."Guidance and homing systems; Space mechanics; Satellites.Includes biblio...

The effect of various missile characteristics on airframe frequency response /

Matthews, Howard F.
McNeill, Walter E., joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Ames Research Center.

On front cover: "January 7, 1952, Declassified December 13, 1957."Includes bibliographical reference...

Effects of flight conditions at booster separation on payload weight in orbit /

Nelson, Richard D.
United States. National Aeronautics and Space Administration.

Cover title."November 1961."Missiles and satellite carriers; Space mechanics.Includes bibliographica...

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...

Investigation toward simplification of missile control systems /

Curfman, Howard J.
Crane, Harold L.
Strass, H. Kurt.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.
United States. National Advisory Committee for Aeronautics.

January 1953

"November 12, 1953."Includes bibliographical references (p. 7).Mode of access: Internet

Predicted shock envelopes about two types of vehicles at large angles of attack /

Kaattari, George E.
United States. National Aeronautics and Space Administration.

Cover title."April 1961."Aerodynamics, missiles and space vehicles; Fluid mechanics.Includes bibliog...

A study of a pilots ability to control during simulated stability augmentation system failures

Sadoff, Melvin.
United States. National Aeronautics and Space Administration.

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

Comparison of two maneuvers for longitudinal range control during atmospheric entry /

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

Cover title."Januery 1962."Aerodynamics, missiles and space vehicles; Atmospheric entry.Includes bib...

A theoretical investigation of the effect of cross-control derivatives on the stability characteristics of airplanes designed for flight at high mach numbers /

Brown, Lawrence W.
United States. National Aeronautics and Space Administration.

Cover title."March 1962."Aerodynamics, aircraft; Stability and control.Includes bibliographical refe...

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...

Preliminary studies of manned satellites wingless configuration : nonlifting /

Faget, Maxime A. (Maxime Allan), 1921-2004.
Buglia, James J.
Garland, Benjamine J.
United States. National Aeronautics and Space Administration.

Cover title."March 1962."Aerodynamics, missiles and space vehicles; Atmospheric entry.Includes bibli...

Numerical analysis of the transient responce of advanced thermal protection systems for atmosphereic entry / Robert T. Swann and Claud M. Pittman.

Swann, Robert T.
Pittman, C. M. (Claud M.)
United States. National Aeronautics and Space Administration.

Cover title."July 1962."Aerodynamics, missiles and space vehicles; Atmospheric entry; Fluid mechanic...

Theoretical investigation of effects of changes in command computations and filter location on response of an automatically controlled interceptor during the attack phase /

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Theoretical investigation of effects of changes in command computations and filter location on response of an automatically controlled interceptor during the attack phase /

Abstract

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