Comparison of theoretical and experimental values for the effective heat of ablation of ammonium chloride /

Boiling heat transfer to liquid hydrogen and nitrogen in forced flow /

Lewis, James P.
Kline, John F.
Goodykoontz, Jack H.
United States. National Aeronautics and Space Administration.

Cover title."September 1962."Fluid mechanics; Propellants; Propulsion system elements; Propulsion sy...

Chemical equilibrium of ablation materials including condensed species /

Stroud, C. W.
Brinkley, Kay L.
United States. National Aeronautics and Space Administration.
Langley Research Center.

Chemical equilibrium of ablation materials including condensed species.Prepared at Langley Research ...

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...

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...

The determination of ablative properties of materials in free-flight ranges /

Savin, Raymond C.
Dahms, Richard G.
Gloria, Hermilo R.
United States. National Aeronautics and Space Administration.

Cover title."June 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...

Determination of local experimental heat-transfer coefficients on combustion side of an ammonia-oxygen rocket /

Liebert, Curt H.
United States. National Aeronautics and Space Administration.

Cover title."September 1961."Propellants; Propulsion system elements; Propulsion systems, liquid-fue...

The performance of ablative materials in a high-energy, partially dissociated, frozen nitrogen stream /

Vojvodich, Nick S.
United States. National Aeronautics and Space Administration.

Cover title."May 1962."Chemistry, organic; Fluid mechanics; Materials, engineering; Structures.Inclu...

Numerical computation of aerodynamic heating of liquid propellants /

Kramer, John L.
Roudebush, William H.
Lowell, Herman H.
Lewis Research Center.

Prepared at Lewis Research Center."April 1960."Cover title.Includes bibliographical references (p. 1...

A thermodynamic analysis of thrust augmentation for nuclear rockets /

Henneberry, Hugh M.
Becker, Roger D.
Corrington, Lester C.
United States. National Aeronautics and Space Administration.

Cover title." March 1961."Propulsion systems, liquid fuel rockets; Propulsion systems, nuclear.Inclu...

An experimental investigation of several ablation materials in an electric-arc-heated air jet

Chapman, Andrew J.
United States. National Aeronautics and Space Administration.

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

Theoretical performance of propellants suitable for electrothermal jet engines /

Jack, John R.
United States. National Aeronautics and Space Administration.

Cover title." April 1961."Propellants; Propulsioin systems, electric; Propulsion systems, theory.Inc...

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...

An experimental investigation of ablating materials at low and high enthalpy potentials /

Rashis, Bernard.
Walton, Thomas E.
United States. National Aeronautics and Space Administration.

"March 1960."Cover title.Includes bibliographical references (p. 12).Mode of access: Internet

Theoretical investigations of the ablation of a glass-type heat protection shield of varied material properties at the stagnation point of a re-entering IRBM /

Adams, Ernst W.
United States. National Aeronautics and Space Administration.

Cover title."January 1961."Atmospheric entry; Materials, other.Includes bibliographical references.M...

Boiling heat transfer to liquid hydrogen and nitrogen in forced flow /

Lewis, James P.
Kline, John F.
Goodykoontz, Jack H.
United States. National Aeronautics and Space Administration.

Cover title."September 1962."Fluid mechanics; Propellants; Propulsion system elements; Propulsion sy...

Chemical equilibrium of ablation materials including condensed species /

Stroud, C. W.
Brinkley, Kay L.
United States. National Aeronautics and Space Administration.
Langley Research Center.

Chemical equilibrium of ablation materials including condensed species.Prepared at Langley Research ...

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...

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...

The determination of ablative properties of materials in free-flight ranges /

Savin, Raymond C.
Dahms, Richard G.
Gloria, Hermilo R.
United States. National Aeronautics and Space Administration.

Cover title."June 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...

Determination of local experimental heat-transfer coefficients on combustion side of an ammonia-oxygen rocket /

Liebert, Curt H.
United States. National Aeronautics and Space Administration.

Cover title."September 1961."Propellants; Propulsion system elements; Propulsion systems, liquid-fue...

The performance of ablative materials in a high-energy, partially dissociated, frozen nitrogen stream /

Vojvodich, Nick S.
United States. National Aeronautics and Space Administration.

Cover title."May 1962."Chemistry, organic; Fluid mechanics; Materials, engineering; Structures.Inclu...

Numerical computation of aerodynamic heating of liquid propellants /

Kramer, John L.
Roudebush, William H.
Lowell, Herman H.
Lewis Research Center.

Prepared at Lewis Research Center."April 1960."Cover title.Includes bibliographical references (p. 1...

A thermodynamic analysis of thrust augmentation for nuclear rockets /

Henneberry, Hugh M.
Becker, Roger D.
Corrington, Lester C.
United States. National Aeronautics and Space Administration.

Cover title." March 1961."Propulsion systems, liquid fuel rockets; Propulsion systems, nuclear.Inclu...

An experimental investigation of several ablation materials in an electric-arc-heated air jet

Chapman, Andrew J.
United States. National Aeronautics and Space Administration.

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

Theoretical performance of propellants suitable for electrothermal jet engines /

Jack, John R.
United States. National Aeronautics and Space Administration.

Cover title." April 1961."Propellants; Propulsioin systems, electric; Propulsion systems, theory.Inc...

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...

An experimental investigation of ablating materials at low and high enthalpy potentials /

Rashis, Bernard.
Walton, Thomas E.
United States. National Aeronautics and Space Administration.

"March 1960."Cover title.Includes bibliographical references (p. 12).Mode of access: Internet

Theoretical investigations of the ablation of a glass-type heat protection shield of varied material properties at the stagnation point of a re-entering IRBM /

Adams, Ernst W.
United States. National Aeronautics and Space Administration.

Cover title."January 1961."Atmospheric entry; Materials, other.Includes bibliographical references.M...

Boiling heat transfer to liquid hydrogen and nitrogen in forced flow /

Lewis, James P.
Kline, John F.
Goodykoontz, Jack H.
United States. National Aeronautics and Space Administration.

Cover title."September 1962."Fluid mechanics; Propellants; Propulsion system elements; Propulsion sy...

Chemical equilibrium of ablation materials including condensed species /

Stroud, C. W.
Brinkley, Kay L.
United States. National Aeronautics and Space Administration.
Langley Research Center.

Chemical equilibrium of ablation materials including condensed species.Prepared at Langley Research ...

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...

Comparison of theoretical and experimental values for the effective heat of ablation of ammonium chloride /

Abstract

Extracted data

Comparison of theoretical and experimental values for the effective heat of ablation of ammonium chloride /

Abstract

Extracted data

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