Theoretical performance of liquid ammonia, hydrazine and mixture of liquid ammonia and hydrazine as fuels with liquid oxygen bifluoride as oxidant for rocket engines

Preliminary investigation of effects of combustion in ram jet on performance of supersonic diffusers.

Schroeder, Albert H.
Connors, James F., joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Lewis Flight Propulsion Laboratory.

On front cover: "December 22, 1948."Title from cover.Includes bibliographical references (p. 6).Mode...

Comparison of experimental and kinetically limited theoretical performance of the hydrogen-flourine propellant system /

Bittker, David A.
United States. National Aeronautics and Space Administration.

Cover title."August 1966."Includes bibliographical references.Mode of access: Internet

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 performance of liquid hydrogen and liquid fluorine in regeneratively cooled rocket engines /

Douglass, H. W.
Price, H. G.
Hennings, G.
Langley Research Center.

January 1959

"November 1959."Cover title.Includes bibliographical references (p. 22-23).Mode of access: Internet

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...

Theoretical performance of diborane as a rocket fuel /

Huff, Vearl N.
Erdmann, Virginia C., joint author.
Calvert, Clyde S., joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Lewis Flight Propulsion Laboratory (Cleveland, OH)

On front cover: "January 10, 1949."Title from cover.Includes bibliographical references (p. 9-10).Mo...

Comparison of hydrazine nitrogen tetroxide and hydrazine chlorine trifluoride in small scale rocket chambers /

Rollbuhler, R. James.
Tomazic, William A.
United States. National Aeronautics and Space Administration.

Cover title."October 1959."Engines, rocket; Fuels, rockets (includes fuel and oxidant); Combustion, ...

Ignition of a hydrogen-oxygen rocket engine by addition of fluorine to the oxidant /

Rollbuhler, R. James.
Straight, David M.
United States. National Aeronautics and Space Administration.

Cover title."July 1962."Propellants; Propulsion system elements; Propulsion systems, liquid-fuel roc...

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...

Experimental performance of a hydrogen-fluorine rocket engine at several chamber pressures and exhaust-nozzle expansion area ratios /

Jones, William L.
Gibb, John W.
Aukerman, Carl A.
Lewis Research Center.

January 1960

"October 1960."Cover title.Includes bibliographical references (p. 20).Mode of access: Internet

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...

Starting of rocket engine at conditions of simulated altitude using crude monoethylaniline and other fuels with mixed acid /

Morrell, Gerald joint author.
Humphrey, Jack C., joint author.
Sloop, John L., joint author.
Ladanyi, Dezso J., joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Lewis Flight Propulsion Laboratory.

On front cover: "July 19, 1950."Includes bibliographical references: p. 16.Mode of access: Internet

Preparation and properties of concentrated boron-hydrocarbon slurry fuels /

Goodman, Irving A.
Fenn, Virginia O., joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Lewis Flight Propulsion Laboratory.

On front cover: "August 6, 1954."Title from cover.Includes bibliographical references: p.14-15.Mode ...

Combined effect of contraction ratio and chamber pressure on the performance of a gaseous hydrogen liquid oxygen combustor for a given propellant weight flow and oxidant fuel ratio /

Hersch, Martin.
United States. National Aeronautics and Space Administration.

Cover title."February 1961."Propulsion system elements; Propulsion systems, liquid-fuel rockets; Pro...

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...

Preliminary investigation of effects of combustion in ram jet on performance of supersonic diffusers.

Schroeder, Albert H.
Connors, James F., joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Lewis Flight Propulsion Laboratory.

On front cover: "December 22, 1948."Title from cover.Includes bibliographical references (p. 6).Mode...

Comparison of experimental and kinetically limited theoretical performance of the hydrogen-flourine propellant system /

Bittker, David A.
United States. National Aeronautics and Space Administration.

Cover title."August 1966."Includes bibliographical references.Mode of access: Internet

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 performance of liquid hydrogen and liquid fluorine in regeneratively cooled rocket engines /

Douglass, H. W.
Price, H. G.
Hennings, G.
Langley Research Center.

January 1959

"November 1959."Cover title.Includes bibliographical references (p. 22-23).Mode of access: Internet

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...

Theoretical performance of diborane as a rocket fuel /

Huff, Vearl N.
Erdmann, Virginia C., joint author.
Calvert, Clyde S., joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Lewis Flight Propulsion Laboratory (Cleveland, OH)

On front cover: "January 10, 1949."Title from cover.Includes bibliographical references (p. 9-10).Mo...

Comparison of hydrazine nitrogen tetroxide and hydrazine chlorine trifluoride in small scale rocket chambers /

Rollbuhler, R. James.
Tomazic, William A.
United States. National Aeronautics and Space Administration.

Cover title."October 1959."Engines, rocket; Fuels, rockets (includes fuel and oxidant); Combustion, ...

Ignition of a hydrogen-oxygen rocket engine by addition of fluorine to the oxidant /

Rollbuhler, R. James.
Straight, David M.
United States. National Aeronautics and Space Administration.

Cover title."July 1962."Propellants; Propulsion system elements; Propulsion systems, liquid-fuel roc...

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...

Experimental performance of a hydrogen-fluorine rocket engine at several chamber pressures and exhaust-nozzle expansion area ratios /

Jones, William L.
Gibb, John W.
Aukerman, Carl A.
Lewis Research Center.

January 1960

"October 1960."Cover title.Includes bibliographical references (p. 20).Mode of access: Internet

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...

Starting of rocket engine at conditions of simulated altitude using crude monoethylaniline and other fuels with mixed acid /

Morrell, Gerald joint author.
Humphrey, Jack C., joint author.
Sloop, John L., joint author.
Ladanyi, Dezso J., joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Lewis Flight Propulsion Laboratory.

On front cover: "July 19, 1950."Includes bibliographical references: p. 16.Mode of access: Internet

Preparation and properties of concentrated boron-hydrocarbon slurry fuels /

Goodman, Irving A.
Fenn, Virginia O., joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Lewis Flight Propulsion Laboratory.

On front cover: "August 6, 1954."Title from cover.Includes bibliographical references: p.14-15.Mode ...

Combined effect of contraction ratio and chamber pressure on the performance of a gaseous hydrogen liquid oxygen combustor for a given propellant weight flow and oxidant fuel ratio /

Hersch, Martin.
United States. National Aeronautics and Space Administration.

Cover title."February 1961."Propulsion system elements; Propulsion systems, liquid-fuel rockets; Pro...

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...

Preliminary investigation of effects of combustion in ram jet on performance of supersonic diffusers.

Schroeder, Albert H.
Connors, James F., joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Lewis Flight Propulsion Laboratory.

On front cover: "December 22, 1948."Title from cover.Includes bibliographical references (p. 6).Mode...

Comparison of experimental and kinetically limited theoretical performance of the hydrogen-flourine propellant system /

Bittker, David A.
United States. National Aeronautics and Space Administration.

Cover title."August 1966."Includes bibliographical references.Mode of access: Internet

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 performance of liquid ammonia, hydrazine and mixture of liquid ammonia and hydrazine as fuels with liquid oxygen bifluoride as oxidant for rocket engines

Abstract

Extracted data

Theoretical performance of liquid ammonia, hydrazine and mixture of liquid ammonia and hydrazine as fuels with liquid oxygen bifluoride as oxidant for rocket engines

Abstract

Extracted data

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