Approximate analysis of G loads and heating during atmospheric entries and passes with constant aerodynamic coefficients Roger W. Luidens.

Analysis of melting boundary layers on decelerating bodies /

Ostrach, Simon.
Hamman, Jesse.
Goldstein, Arthur W.
United States. National Aeronautics and Space Administration.

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

Static aerodynamic characteristics of a 1/9-scale model of the escape and exit configurations of the Project Mercury spacecraft at Mach numbers from 2.30 to 4.65 /

Fournier, Roger H.
Langley Research Center.

January 1962

"September 1962."Cover title.Includes bibliographical references (p. 7).Mode of access: Internet

Calculated mode shapes and pressure distributions at flutter for a highly tapered horizontal tail in subsonic flow /

Hunt, Gerald L.
Walberg, Gerald D.
United States. National Aeronautics and Space Administration.

Cover title."April 1962."Aerodynamics, aircraft; Stresses and loads.Includes bibliographical referen...

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 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...

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

Wells, William R.
McLellan, Charles H.
United States. National Aeronautics and Space Administration.

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

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...

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...

Prospects for obtaining aerodynamic heating results from analysis of meteor flight data /

Allen, H. Julian (Harry Julian), 1910-
James, Nataline A.
Ames Research Center.

Prepared at Ames Research Center."July 1964"--Cover.Includes bibliographical references (p. 53-56).M...

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...

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...

Analysis of radiative heat transfer for large objects at meteoric speeds /

Yoshikawa, Kenneth K.
Ames Research Center.
United States. National Aeronautics and Space Administration.

January 1967

Cover title."June 1967."Includes bibliographical references (p. 84-86).Includes bibliographical refe...

The Aerodynamics of bodies in a rarefied ionized gas with applications to spacecraft environmental dynamics /

Stone, Nobie H.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
George C. Marshall Space Flight Center.

January 1981

"November 1981"--Cover."George C. Marshall Space Flight Center."Includes bibliographical references....

An approximate analysis of film cooling on blunt bodies by gas injection near the stagnation point. /

Swenson, Byron L.
United States. National Aeronautics and Space Administration.

Cover title."September 1961."Aerodynamics, missiles and space vehicles; Fluid mechanics.Includes bib...

Analysis of melting boundary layers on decelerating bodies /

Ostrach, Simon.
Hamman, Jesse.
Goldstein, Arthur W.
United States. National Aeronautics and Space Administration.

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

Static aerodynamic characteristics of a 1/9-scale model of the escape and exit configurations of the Project Mercury spacecraft at Mach numbers from 2.30 to 4.65 /

Fournier, Roger H.
Langley Research Center.

January 1962

"September 1962."Cover title.Includes bibliographical references (p. 7).Mode of access: Internet

Calculated mode shapes and pressure distributions at flutter for a highly tapered horizontal tail in subsonic flow /

Hunt, Gerald L.
Walberg, Gerald D.
United States. National Aeronautics and Space Administration.

Cover title."April 1962."Aerodynamics, aircraft; Stresses and loads.Includes bibliographical referen...

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 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...

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

Wells, William R.
McLellan, Charles H.
United States. National Aeronautics and Space Administration.

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

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...

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...

Prospects for obtaining aerodynamic heating results from analysis of meteor flight data /

Allen, H. Julian (Harry Julian), 1910-
James, Nataline A.
Ames Research Center.

Prepared at Ames Research Center."July 1964"--Cover.Includes bibliographical references (p. 53-56).M...

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...

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...

Analysis of radiative heat transfer for large objects at meteoric speeds /

Yoshikawa, Kenneth K.
Ames Research Center.
United States. National Aeronautics and Space Administration.

January 1967

Cover title."June 1967."Includes bibliographical references (p. 84-86).Includes bibliographical refe...

The Aerodynamics of bodies in a rarefied ionized gas with applications to spacecraft environmental dynamics /

Stone, Nobie H.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
George C. Marshall Space Flight Center.

January 1981

"November 1981"--Cover."George C. Marshall Space Flight Center."Includes bibliographical references....

An approximate analysis of film cooling on blunt bodies by gas injection near the stagnation point. /

Swenson, Byron L.
United States. National Aeronautics and Space Administration.

Cover title."September 1961."Aerodynamics, missiles and space vehicles; Fluid mechanics.Includes bib...

Analysis of melting boundary layers on decelerating bodies /

Ostrach, Simon.
Hamman, Jesse.
Goldstein, Arthur W.
United States. National Aeronautics and Space Administration.

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

Static aerodynamic characteristics of a 1/9-scale model of the escape and exit configurations of the Project Mercury spacecraft at Mach numbers from 2.30 to 4.65 /

Fournier, Roger H.
Langley Research Center.

January 1962

"September 1962."Cover title.Includes bibliographical references (p. 7).Mode of access: Internet

Calculated mode shapes and pressure distributions at flutter for a highly tapered horizontal tail in subsonic flow /

Hunt, Gerald L.
Walberg, Gerald D.
United States. National Aeronautics and Space Administration.

Cover title."April 1962."Aerodynamics, aircraft; Stresses and loads.Includes bibliographical referen...

Approximate analysis of G loads and heating during atmospheric entries and passes with constant aerodynamic coefficients Roger W. Luidens.

Abstract

Extracted data

Approximate analysis of G loads and heating during atmospheric entries and passes with constant aerodynamic coefficients Roger W. Luidens.

Abstract

Extracted data

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