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

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 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...

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...

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....

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...

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...

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

An optimization of powerplant paramemters for orbital-launch nuclear rockets /

Johnson, Paul G.
Smith, Roger L.
United States. National Aeronautics and Space Administration.

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

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...

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

Digital codes for design and evaluation of convectively cooled rocket nozzle with application to nuclear-type rocket /

Rohde, John E.
Derderian, George.
Duscha, Rudolph A.
United States. National Aeronautics and Space Administration.

Cover title."January 1967."Includes bibliographical references.Mode of access: Internet

Analysis of heat transfer and pressure drop for a gas flowing through a set of multiple parallel flat plates at high temperatures

Einstein, Thomas H.
United States. National Aeronautics and Space Administration.

Cover title."December 1961."Fluid mechanics; Propulsion system elements; Propulsion systems, nuclear...

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...

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...

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

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 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...

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...

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....

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...

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...

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

An optimization of powerplant paramemters for orbital-launch nuclear rockets /

Johnson, Paul G.
Smith, Roger L.
United States. National Aeronautics and Space Administration.

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

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...

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

Digital codes for design and evaluation of convectively cooled rocket nozzle with application to nuclear-type rocket /

Rohde, John E.
Derderian, George.
Duscha, Rudolph A.
United States. National Aeronautics and Space Administration.

Cover title."January 1967."Includes bibliographical references.Mode of access: Internet

Analysis of heat transfer and pressure drop for a gas flowing through a set of multiple parallel flat plates at high temperatures

Einstein, Thomas H.
United States. National Aeronautics and Space Administration.

Cover title."December 1961."Fluid mechanics; Propulsion system elements; Propulsion systems, nuclear...

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...

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...

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

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 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...

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...

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

Abstract

Extracted data

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

Abstract

Extracted data

Related items

Related items