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

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...

Design and calibration of an arc-heated, hypersonic, low-density wind tunnel

Weitmann, Ruth N.
United States. National Aeronautics and Space Administration.

Cover title."August 1962."Aerodynamics, missiles and space vehicles; Atmospheric entry; Chemistry, p...

Control of a large launch vehicle with limited thrust vectoring in the presence of winds /

Collins, Dennis F. (Dennis Francis), 1936-
Morgan, Homer G.
Langley Research Center.

Prepared at Langley Research Center."August 1963."Cover title.Includes bibliographical references (p...

The effect of lateral- and longitudinal-range control on allowable entry conditions for a point return from space /

Boissevain, Alfred G.
United States. National Aeronautics and Space Administration.

Cover title."July 1961."Atmospheric entry; Space mechanics; Space vehicles.Includes bibliographical ...

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...

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...

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...

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...

An analytical method for studying the lateral motion of atmosphere entry vehicles. /

Slye, Robert E.
United States. National Aeronautics and Space Administration.

Cover title."September 1960."Atmospheric entry; Guidance and homing systems; Navigation and navigati...

Low-speed longitudinal aerodynamic characteristics associated with a series of low-aspect-ration wings having variations in leading contour / Bernard Spencer Jr. and Alexander D. Hammond.

Spencer, Bernard.
Hammond, Alexander D.
United States. National Aeronautics and Space Administration.

Cover title."September 1962."Aerodynamics, missiles and space vehicles; Atmospheric entry; Satellite...

Free-flight of fifth-stage entry vehicle at mach numbers of 5 and 17 /

Kirk, Donn B.
Miller, Robert J.
United States. National Aeronautics and Space Administration.

Cover title."October 1962."Aerodynamics, missiles and space vehicles; Atmospheric entry; Stability a...

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...

Motions of a short 10 degree blunted cone entering a Martian atmosphere at arbitrary angles of attack and arbitrary pitching rates /

Peterson, Victor L.
United States. National Aeronautics and Space Administration.

Cover title."May 1962."Aerodynamics, missiles and space vehicles; Atmospheric entry; Fluid mechanics...

Wind-tunnel tests of a series of 18-foot-diameter parachutes with extendable flaps /

Gamse, Berl.
Yaggy, Paul F.
United States. National Aeronautics and Space Administration.

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

Interference effects of canard controls on the longitudinal aerodynamic characteristics of a winged body at Mach 10 /

Brooks, Cuyler W.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."April 1968."Includes bibliographical references (p. 11).Mode of access: Internet

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...

Design and calibration of an arc-heated, hypersonic, low-density wind tunnel

Weitmann, Ruth N.
United States. National Aeronautics and Space Administration.

Cover title."August 1962."Aerodynamics, missiles and space vehicles; Atmospheric entry; Chemistry, p...

Control of a large launch vehicle with limited thrust vectoring in the presence of winds /

Collins, Dennis F. (Dennis Francis), 1936-
Morgan, Homer G.
Langley Research Center.

Prepared at Langley Research Center."August 1963."Cover title.Includes bibliographical references (p...

The effect of lateral- and longitudinal-range control on allowable entry conditions for a point return from space /

Boissevain, Alfred G.
United States. National Aeronautics and Space Administration.

Cover title."July 1961."Atmospheric entry; Space mechanics; Space vehicles.Includes bibliographical ...

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...

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...

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...

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...

An analytical method for studying the lateral motion of atmosphere entry vehicles. /

Slye, Robert E.
United States. National Aeronautics and Space Administration.

Cover title."September 1960."Atmospheric entry; Guidance and homing systems; Navigation and navigati...

Low-speed longitudinal aerodynamic characteristics associated with a series of low-aspect-ration wings having variations in leading contour / Bernard Spencer Jr. and Alexander D. Hammond.

Spencer, Bernard.
Hammond, Alexander D.
United States. National Aeronautics and Space Administration.

Cover title."September 1962."Aerodynamics, missiles and space vehicles; Atmospheric entry; Satellite...

Free-flight of fifth-stage entry vehicle at mach numbers of 5 and 17 /

Kirk, Donn B.
Miller, Robert J.
United States. National Aeronautics and Space Administration.

Cover title."October 1962."Aerodynamics, missiles and space vehicles; Atmospheric entry; Stability a...

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...

Motions of a short 10 degree blunted cone entering a Martian atmosphere at arbitrary angles of attack and arbitrary pitching rates /

Peterson, Victor L.
United States. National Aeronautics and Space Administration.

Cover title."May 1962."Aerodynamics, missiles and space vehicles; Atmospheric entry; Fluid mechanics...

Wind-tunnel tests of a series of 18-foot-diameter parachutes with extendable flaps /

Gamse, Berl.
Yaggy, Paul F.
United States. National Aeronautics and Space Administration.

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

Interference effects of canard controls on the longitudinal aerodynamic characteristics of a winged body at Mach 10 /

Brooks, Cuyler W.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."April 1968."Includes bibliographical references (p. 11).Mode of access: Internet

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...

Design and calibration of an arc-heated, hypersonic, low-density wind tunnel

Weitmann, Ruth N.
United States. National Aeronautics and Space Administration.

Cover title."August 1962."Aerodynamics, missiles and space vehicles; Atmospheric entry; Chemistry, p...

Control of a large launch vehicle with limited thrust vectoring in the presence of winds /

Collins, Dennis F. (Dennis Francis), 1936-
Morgan, Homer G.
Langley Research Center.

Prepared at Langley Research Center."August 1963."Cover title.Includes bibliographical references (p...

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

Abstract

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

Abstract

Extracted data

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