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

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...

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...

Investigation of the dynamics of water rejection from a hydrogen-oxygen fuel cell to a hydrogen stream /

Prokopius, Paul R.
Hagedorn, Norman H.
Lewis Research Center.

Prepared at Lewis Research Center."October 1967"--Cover.Includes bibliographical references (p. 24)....

Experimental heat-transfer study of a regeneratively cooled hydrogen-fluorine rocket engine at low chamber pressure /

Curren, Arthur N.
Lewis Research Center.

Prepared at Lewis Research Center."September 1967"--Cover.Includes bibliographical references (p. 30...

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

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...

Heat-transfer coefficients for hydrogen flowing through parallel hexagonal passages at surface temperatures to 2275 K /

Slaby, Jack G.
Mattson, William F.
Lewis Research Center.

Prepared at Lewis Research Center."December 1968"--Cover.Includes bibliographical references (p. 22)...

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...

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...

Experimental heat-transfer results for cryogenic hydrogen flowing in tubes at subcritical and supercritical pressures to 800 pounds per square inch absolute /

Hendricks, Robert C.
Lewis Research Center.

Prepared at Lewis Research Center."March 1966"--Cover.Includes bibliographical references (p. 142-14...

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

Adams, D. W.
Weiland, W. F., Jr.

September 1969

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

Heat transfer to cryogenic hydrogen flowing turbulently in straight and curved tubes at high heat fluxes.

Aerojet-General Corporation.
United States. National Aeronautics and Space Administration.

January 1967

"February 1967."Includes bibliographical references."Prepared under contract no.Mode of access: Inte...

Thermodynamic properties of hydrogen from room temperature to 100,000 degrees K /

Rosenbaum, Burt M.
Levitt, Leo.
United States. National Aeronautics and Space Administration.

Cover title."January 1962."Fluid mechanics;Physics, atomic and molecular; Physics, theoretical; Prop...

Local turbulent heat transfer for water in entrance regions of tubes with various unheated starting lengths /

Stone, James R.
Lewis Research Center.

Prepared at Lewis Research Center."November 1965"--Cover.Includes bibliographical references (p. 17)...

Analysis of the transient radiation heat transfer of an uncooled rocket engine operating outside Earth's atmosphere /

Robbins, William H.
Lewis Research Center.

January 1959

"NASA TN D-62.""Lewis Research Center, Cleveland, Ohio.""December 1959."Title from cover.Includes bi...

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...

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...

Investigation of the dynamics of water rejection from a hydrogen-oxygen fuel cell to a hydrogen stream /

Prokopius, Paul R.
Hagedorn, Norman H.
Lewis Research Center.

Prepared at Lewis Research Center."October 1967"--Cover.Includes bibliographical references (p. 24)....

Experimental heat-transfer study of a regeneratively cooled hydrogen-fluorine rocket engine at low chamber pressure /

Curren, Arthur N.
Lewis Research Center.

Prepared at Lewis Research Center."September 1967"--Cover.Includes bibliographical references (p. 30...

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

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...

Heat-transfer coefficients for hydrogen flowing through parallel hexagonal passages at surface temperatures to 2275 K /

Slaby, Jack G.
Mattson, William F.
Lewis Research Center.

Prepared at Lewis Research Center."December 1968"--Cover.Includes bibliographical references (p. 22)...

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...

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...

Experimental heat-transfer results for cryogenic hydrogen flowing in tubes at subcritical and supercritical pressures to 800 pounds per square inch absolute /

Hendricks, Robert C.
Lewis Research Center.

Prepared at Lewis Research Center."March 1966"--Cover.Includes bibliographical references (p. 142-14...

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

Adams, D. W.
Weiland, W. F., Jr.

September 1969

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

Heat transfer to cryogenic hydrogen flowing turbulently in straight and curved tubes at high heat fluxes.

Aerojet-General Corporation.
United States. National Aeronautics and Space Administration.

January 1967

"February 1967."Includes bibliographical references."Prepared under contract no.Mode of access: Inte...

Thermodynamic properties of hydrogen from room temperature to 100,000 degrees K /

Rosenbaum, Burt M.
Levitt, Leo.
United States. National Aeronautics and Space Administration.

Cover title."January 1962."Fluid mechanics;Physics, atomic and molecular; Physics, theoretical; Prop...

Local turbulent heat transfer for water in entrance regions of tubes with various unheated starting lengths /

Stone, James R.
Lewis Research Center.

Prepared at Lewis Research Center."November 1965"--Cover.Includes bibliographical references (p. 17)...

Analysis of the transient radiation heat transfer of an uncooled rocket engine operating outside Earth's atmosphere /

Robbins, William H.
Lewis Research Center.

January 1959

"NASA TN D-62.""Lewis Research Center, Cleveland, Ohio.""December 1959."Title from cover.Includes bi...

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...

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...

Investigation of the dynamics of water rejection from a hydrogen-oxygen fuel cell to a hydrogen stream /

Prokopius, Paul R.
Hagedorn, Norman H.
Lewis Research Center.

Prepared at Lewis Research Center."October 1967"--Cover.Includes bibliographical references (p. 24)....

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

Abstract

Extracted data

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

Abstract

Extracted data

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