Transfer of cryogenic fluids by an expulsion-bag technique. /

An analysis of thermal radiation heat transfer in a nuclear-rocket nozzle /

Robbins, William H.
United States. National Aeronautics and Space Administration.

Cover title."January 1961."Propulsion systems, nuclear.Includes bibliographical references.Mode of a...

Analysis, feasibility, and wall-temperature distribution of a radiation-cooled nuclear-rocket nozzle. /

Robbins, William H.
Todd, Carroll A.
United States. National Aeronautics and Space Administration.

Cover title."January 1962."Fluid mechanics; Propulsion system elements; Propulsion systems, nuclear....

Analytical performance characteristics and outlet flow conditions of constant and variable lead helical inducers for cryogenic pumps /

Montgomery, John C.
United States. National Aeronautics and Space Administration.

Cover title."March 1961."Fluid mechanics; Propulsioin system elements; Propulsion systems, liquid-fu...

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...

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...

Experimental damping of liquid oscillations in a spherical tank by positive-expulsion bags and diaphragms /

Stofan, Andrew J.
Pavli, Albert J.
United States. National Aeronautics and Space Administration.

Cover title."July 1962."Fluid mechanics; Launching dynamics; Propellants; Propulsion system elements...

Management of cryogenic propellants in a full-scale orbiting space vehicle /

Lacovic, Raymond F.
Lewis Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."May 1968."Includes bibliographical references (p. 32).Mode of access: Internet

An investigation of the liquid level at the wall of a spinning tank

Winch, David M.
United States. National Aeronautics and Space Administration.

Cover title."August 1962."Fluid mechanics; Propulsion systems, liquid-fuel rockets.Includes bibliogr...

Experimental performance of nozzles having area ratios up to 300 on JP-4 fuel - liquid-oxygen rocket engine. /

Lovell, J. Calvin
Samanich, Nick E.
United States. National Aeronautics and Space Administration.

Abstract:Cover title."June 1961."Aerodynamics, missiles and space vehicles; Propulsion system elemen...

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...

Annular internal-external-expansion rocket nozzles for large booster applications /

Connors, James F.
Mitchell, Glenn A.
Cubbison, Robert W.
United States. National Aeronautics and Space Administration.

Cover title."September 1961."Aerodynamics, missiles and space vehicles; Missiles and satellite carri...

Potential-flow analysis of unsteady outflow from a tank and its effect on the dynamics of a fluid system

Roudebush, William H.
Pinkel, I. Irving.
United States. National Aeronautics and Space Administration.

Cover title."June 1962."Fluid mechanics; Propulsion system elements; Propulsion systems, liquid-fuel...

Ignition of hydrogen-oxygen rocket combustor with chlorine trifluoride and triethylaluminum /

Gregory, John W.
Straight, David M.
United States. National Aeronautics and Space Administration.

Cover title."April 1961."Materials, other; Propulsion system elements; Propulsion systems, liquid fu...

Heat- and mass-transfer characteristics of an axial-flow liquid-core nuclear rocket employing radiation heat transfer /

Ragsdale, Robert G.
Donovan, Leo F.
Kascak, Albert F.
United States. National Aeronautics and Space Administration.

January 1967

Cover title."August 1967."Includes bibliographical references (p. 31-32).Mode of access: Internet

A preliminary study of the use of finite-thrust engines for abort during launch of space vehicles /

McGowan, William A.
United States. National Aeronautics and Space Administration.

Cover title."December 1961."Atmospheric entry; Space mechanics; Space vehicles.Includes bibliographi...

An analysis of thermal radiation heat transfer in a nuclear-rocket nozzle /

Robbins, William H.
United States. National Aeronautics and Space Administration.

Cover title."January 1961."Propulsion systems, nuclear.Includes bibliographical references.Mode of a...

Analysis, feasibility, and wall-temperature distribution of a radiation-cooled nuclear-rocket nozzle. /

Robbins, William H.
Todd, Carroll A.
United States. National Aeronautics and Space Administration.

Cover title."January 1962."Fluid mechanics; Propulsion system elements; Propulsion systems, nuclear....

Analytical performance characteristics and outlet flow conditions of constant and variable lead helical inducers for cryogenic pumps /

Montgomery, John C.
United States. National Aeronautics and Space Administration.

Cover title."March 1961."Fluid mechanics; Propulsioin system elements; Propulsion systems, liquid-fu...

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...

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...

Experimental damping of liquid oscillations in a spherical tank by positive-expulsion bags and diaphragms /

Stofan, Andrew J.
Pavli, Albert J.
United States. National Aeronautics and Space Administration.

Cover title."July 1962."Fluid mechanics; Launching dynamics; Propellants; Propulsion system elements...

Management of cryogenic propellants in a full-scale orbiting space vehicle /

Lacovic, Raymond F.
Lewis Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."May 1968."Includes bibliographical references (p. 32).Mode of access: Internet

An investigation of the liquid level at the wall of a spinning tank

Winch, David M.
United States. National Aeronautics and Space Administration.

Cover title."August 1962."Fluid mechanics; Propulsion systems, liquid-fuel rockets.Includes bibliogr...

Experimental performance of nozzles having area ratios up to 300 on JP-4 fuel - liquid-oxygen rocket engine. /

Lovell, J. Calvin
Samanich, Nick E.
United States. National Aeronautics and Space Administration.

Abstract:Cover title."June 1961."Aerodynamics, missiles and space vehicles; Propulsion system elemen...

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...

Annular internal-external-expansion rocket nozzles for large booster applications /

Connors, James F.
Mitchell, Glenn A.
Cubbison, Robert W.
United States. National Aeronautics and Space Administration.

Cover title."September 1961."Aerodynamics, missiles and space vehicles; Missiles and satellite carri...

Potential-flow analysis of unsteady outflow from a tank and its effect on the dynamics of a fluid system

Roudebush, William H.
Pinkel, I. Irving.
United States. National Aeronautics and Space Administration.

Cover title."June 1962."Fluid mechanics; Propulsion system elements; Propulsion systems, liquid-fuel...

Ignition of hydrogen-oxygen rocket combustor with chlorine trifluoride and triethylaluminum /

Gregory, John W.
Straight, David M.
United States. National Aeronautics and Space Administration.

Cover title."April 1961."Materials, other; Propulsion system elements; Propulsion systems, liquid fu...

Heat- and mass-transfer characteristics of an axial-flow liquid-core nuclear rocket employing radiation heat transfer /

Ragsdale, Robert G.
Donovan, Leo F.
Kascak, Albert F.
United States. National Aeronautics and Space Administration.

January 1967

Cover title."August 1967."Includes bibliographical references (p. 31-32).Mode of access: Internet

A preliminary study of the use of finite-thrust engines for abort during launch of space vehicles /

McGowan, William A.
United States. National Aeronautics and Space Administration.

Cover title."December 1961."Atmospheric entry; Space mechanics; Space vehicles.Includes bibliographi...

An analysis of thermal radiation heat transfer in a nuclear-rocket nozzle /

Robbins, William H.
United States. National Aeronautics and Space Administration.

Cover title."January 1961."Propulsion systems, nuclear.Includes bibliographical references.Mode of a...

Analysis, feasibility, and wall-temperature distribution of a radiation-cooled nuclear-rocket nozzle. /

Robbins, William H.
Todd, Carroll A.
United States. National Aeronautics and Space Administration.

Cover title."January 1962."Fluid mechanics; Propulsion system elements; Propulsion systems, nuclear....

Analytical performance characteristics and outlet flow conditions of constant and variable lead helical inducers for cryogenic pumps /

Montgomery, John C.
United States. National Aeronautics and Space Administration.

Cover title."March 1961."Fluid mechanics; Propulsioin system elements; Propulsion systems, liquid-fu...

Transfer of cryogenic fluids by an expulsion-bag technique. /

Abstract

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Transfer of cryogenic fluids by an expulsion-bag technique. /

Abstract

Extracted data

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