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

Analysis of topping and bleed turbopump units for hydrogen-propelled nuclear rockets /

Evans, David G.
Crouse, James E.
Lewis Research Center.

January 1960

"June 1960."Cover title.Includes bibliographical references (p. 24).Mode of access: Internet

Experimental evaluation of heat transfer on a 1030:1 area ratio rocket nozzle /

Kacynski, Kenneth J.
Smith, Tamara A.
Pavli, Albert J.
Lewis Research Center.

January 1987

Prepared at Lewis Research Center."August 1987"--Cover.Includes bibliographical references (p. 24).M...

Feasibility of optimizing nozzle performance for orbital-launch nuclear rockets

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

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

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...

Theoretical investigation of radiant heat transfer in the fuel region of a gaseous nuclear rocket engine /

Kesten, A. S.
Krascella, N. L.

"January 1967"--cover.Includes bibliographical references.Prepared by United Aircraft Corporation.Mo...

Cooldown characteristics of regenerative nozzle used in full-scale, cold-flow, nuclear rocket test facility /

Turney, George E.
Cox, Eileen.
Lewis Research Center.
United States. National Aeronautics and Space Administration.

January 1967

Cover title."May 1967."Includes bibliographical references (57-58).Mode of access: Internet

Heat-transfer characteristics of a water-to-cryogenic-hydrogen heat exchanger /

Weiland, Walter F.
Adams, Donald W.
United States. National Aeronautics and Space Administration.
Lewis Research Center.

Heat transfer characteristics of water/cryogenic hydrogen heat exchanger for nuclear rocket reactor....

Simulation of gaseous core nuclear rocket mixing characteristics using cold and arc heated flows /

Williams, Peter M.
Grey, Jerry.
Lewis Research Center.
United States. National Aeronautics and Space Administration.

January 1967

"June, 1967."Includes bibliographical references."Prepared under contract no.Mode of access: Interne...

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...

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...

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...

Nuclear radiation transfer and heat deposition rates in liquid hydrogen /

Burrell, M. O. (Martin Omar), 1925-
George C. Marshall Space Flight Center.

Prepared at George C. Marshall Space Flight Center."August 1962."Cover title.Includes bibliographica...

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....

Heat-transfer measurements on a blunt spherical-segment nose to a Mach number of 15.1 and flight performance of the rocket-propelled model to a Mach number of 17.8 /

Rumsey, Charles B.
Lee, Dorothy B.
Langley Research Center.

January 1959

"November 1959."Cover title.Includes bibliographical references (p. 17-18).Mode of access: Internet

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...

Analysis of topping and bleed turbopump units for hydrogen-propelled nuclear rockets /

Evans, David G.
Crouse, James E.
Lewis Research Center.

January 1960

"June 1960."Cover title.Includes bibliographical references (p. 24).Mode of access: Internet

Experimental evaluation of heat transfer on a 1030:1 area ratio rocket nozzle /

Kacynski, Kenneth J.
Smith, Tamara A.
Pavli, Albert J.
Lewis Research Center.

January 1987

Prepared at Lewis Research Center."August 1987"--Cover.Includes bibliographical references (p. 24).M...

Feasibility of optimizing nozzle performance for orbital-launch nuclear rockets

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

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

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...

Theoretical investigation of radiant heat transfer in the fuel region of a gaseous nuclear rocket engine /

Kesten, A. S.
Krascella, N. L.

"January 1967"--cover.Includes bibliographical references.Prepared by United Aircraft Corporation.Mo...

Cooldown characteristics of regenerative nozzle used in full-scale, cold-flow, nuclear rocket test facility /

Turney, George E.
Cox, Eileen.
Lewis Research Center.
United States. National Aeronautics and Space Administration.

January 1967

Cover title."May 1967."Includes bibliographical references (57-58).Mode of access: Internet

Heat-transfer characteristics of a water-to-cryogenic-hydrogen heat exchanger /

Weiland, Walter F.
Adams, Donald W.
United States. National Aeronautics and Space Administration.
Lewis Research Center.

Heat transfer characteristics of water/cryogenic hydrogen heat exchanger for nuclear rocket reactor....

Simulation of gaseous core nuclear rocket mixing characteristics using cold and arc heated flows /

Williams, Peter M.
Grey, Jerry.
Lewis Research Center.
United States. National Aeronautics and Space Administration.

January 1967

"June, 1967."Includes bibliographical references."Prepared under contract no.Mode of access: Interne...

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...

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...

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...

Nuclear radiation transfer and heat deposition rates in liquid hydrogen /

Burrell, M. O. (Martin Omar), 1925-
George C. Marshall Space Flight Center.

Prepared at George C. Marshall Space Flight Center."August 1962."Cover title.Includes bibliographica...

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....

Heat-transfer measurements on a blunt spherical-segment nose to a Mach number of 15.1 and flight performance of the rocket-propelled model to a Mach number of 17.8 /

Rumsey, Charles B.
Lee, Dorothy B.
Langley Research Center.

January 1959

"November 1959."Cover title.Includes bibliographical references (p. 17-18).Mode of access: Internet

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...

Analysis of topping and bleed turbopump units for hydrogen-propelled nuclear rockets /

Evans, David G.
Crouse, James E.
Lewis Research Center.

January 1960

"June 1960."Cover title.Includes bibliographical references (p. 24).Mode of access: Internet

Experimental evaluation of heat transfer on a 1030:1 area ratio rocket nozzle /

Kacynski, Kenneth J.
Smith, Tamara A.
Pavli, Albert J.
Lewis Research Center.

January 1987

Prepared at Lewis Research Center."August 1987"--Cover.Includes bibliographical references (p. 24).M...

Feasibility of optimizing nozzle performance for orbital-launch nuclear rockets

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

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

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

Abstract

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

Abstract

Extracted data

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