One-dimensional heat conduction through the skin of a vehicle upon entering a planetary atmosphere at constant velocity and entry angle /

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...

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...

Theoretical analysis of effects of ablation on heat transfer to an arbitrary axisymmetric body /

Swann, Robert T.
South, Jerry C. (Jerry Curtis), 1935-
United States. National Aeronautics and Space Administration.

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

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...

Experimental and theoretical study of heat conduction for air up to 5000 degrees F /

Peng, Tzy-Cheng.
Ahtye, Warren F.
United States. National Aeronautics and Space Administration.

Cover title."February 1961."Aerodynamics, missiles and space vehicles; Chemical engineering; Chemist...

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...

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...

Local aerodynamic heat transfer and boundary-layer transition on roughened sphere-ellipsoid bodies at mach number 3.0/

Deveikis, William D.
Walker, Robert W.
United States. National Aeronautics and Space Administration.

Cover title."August 1961."Major NASA subject terms: Aerodynamics, missiles and space vehicles; Fluid...

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...

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...

Aerodynamic heating of conical entry vehicles at speeds in excess of earth parabolic speed /

Allen, H. Jullian.
United States. National Aeronautics and Space Administration.
Ames Research Center.

January 1963

"N6412107"--Cover."Dec 1963"--Cover.Includes bibliographical references (p. 57-60).Mode of access: I...

Laminar heat-transfer and pressure-distribution studies on a series of reentry nose shapes at a mach number of 19.4 in helium. /

Wagner, Richard D.
Henderson, Arthur, 1922-
Pine, W. Clint.
United States. National Aeronautics and Space Administration.

Cover title."June 1961."Aerodynamics, missiles and space vehicles; Fluid mechanics.Includes bibliogr...

Surface-temperature distribution on thin-walled bodies subjected to solar radiation in interplanetary space /

Nichols, Lester D.
United States. National Aeronautics and Space Administration.

Cover title."October 1961."Fluid mechanics; Propulsion system elements; Satellites; Space vehicles; ...

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...

Hot-wire heat-loss characteristics and anemometry in subsonic continuum and slip flow /

Boltz, Frederick W.
United States. National Aeronautics and Space Administration.

Cover title."February 1961."Aerodynamics, aircraft; Aerodynamics, missiles and space vehicles; Fluid...

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...

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...

Theoretical analysis of effects of ablation on heat transfer to an arbitrary axisymmetric body /

Swann, Robert T.
South, Jerry C. (Jerry Curtis), 1935-
United States. National Aeronautics and Space Administration.

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

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...

Experimental and theoretical study of heat conduction for air up to 5000 degrees F /

Peng, Tzy-Cheng.
Ahtye, Warren F.
United States. National Aeronautics and Space Administration.

Cover title."February 1961."Aerodynamics, missiles and space vehicles; Chemical engineering; Chemist...

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...

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...

Local aerodynamic heat transfer and boundary-layer transition on roughened sphere-ellipsoid bodies at mach number 3.0/

Deveikis, William D.
Walker, Robert W.
United States. National Aeronautics and Space Administration.

Cover title."August 1961."Major NASA subject terms: Aerodynamics, missiles and space vehicles; Fluid...

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...

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...

Aerodynamic heating of conical entry vehicles at speeds in excess of earth parabolic speed /

Allen, H. Jullian.
United States. National Aeronautics and Space Administration.
Ames Research Center.

January 1963

"N6412107"--Cover."Dec 1963"--Cover.Includes bibliographical references (p. 57-60).Mode of access: I...

Laminar heat-transfer and pressure-distribution studies on a series of reentry nose shapes at a mach number of 19.4 in helium. /

Wagner, Richard D.
Henderson, Arthur, 1922-
Pine, W. Clint.
United States. National Aeronautics and Space Administration.

Cover title."June 1961."Aerodynamics, missiles and space vehicles; Fluid mechanics.Includes bibliogr...

Surface-temperature distribution on thin-walled bodies subjected to solar radiation in interplanetary space /

Nichols, Lester D.
United States. National Aeronautics and Space Administration.

Cover title."October 1961."Fluid mechanics; Propulsion system elements; Satellites; Space vehicles; ...

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...

Hot-wire heat-loss characteristics and anemometry in subsonic continuum and slip flow /

Boltz, Frederick W.
United States. National Aeronautics and Space Administration.

Cover title."February 1961."Aerodynamics, aircraft; Aerodynamics, missiles and space vehicles; Fluid...

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...

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...

Theoretical analysis of effects of ablation on heat transfer to an arbitrary axisymmetric body /

Swann, Robert T.
South, Jerry C. (Jerry Curtis), 1935-
United States. National Aeronautics and Space Administration.

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

One-dimensional heat conduction through the skin of a vehicle upon entering a planetary atmosphere at constant velocity and entry angle /

Abstract

Extracted data

One-dimensional heat conduction through the skin of a vehicle upon entering a planetary atmosphere at constant velocity and entry angle /

Abstract

Extracted data

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