Cold-air performance evaluation of scale model oxidizer pump-drive turbine for the M-1 hydrogen-oxygen rocket engine.

Performance study of a piston-type pump for liquid hydrogen /

Biermann, Arnold E.
Shinko, William G.
Lewis Research Center.

January 1960

"NASA TN D-276.""Lewis Research Center, Cleveland, Ohio.""March 1960."Cover title.Includes bibliogra...

Steady-state performance of a modified Rankine cycle system using water /

Fenn, David B.
Gutierrez, Orlando A.
Coe, Harold H.
Lewis Research Center.

Prepared at Lewis Research Center."March 1966"--Cover.Includes bibliographical references (p. 18).Mo...

Calculations of the performance of a compression-ignition engine-compressor turbine combination.

Mendelson, Alexander.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Aircraft Engine Research Laboratory.

Prepared at the Aircraft Engine Research Laboratory, Cleveland, Ohio.On front cover: "February 3, 19...

Cold-air performance evaluation of scale model oxidizer pump-drive turbine for the M-1 hydrogen-oxygen rocket engine.

Stabe, Roy G.
Kline, John F.
Lewis Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."February 1968."Includes bibliographical references (p. 19-20).Mode of access: Internet

Research turbine for high-temperature core engine application /

Szanca, Edward M.
Lewis Research Center.

January 1974

Prepared at Lewis Research Center.Cover title.Includes bibliographical references.1. Cold-air overal...

Cold-air investigation of 4 1/2-stage turbine with stage-loading factor of 4.66 and high specific work output : II - stage group performance /

Whitney, Warren J.
Lewis Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1980

"June 1980"--Cover."Lewis Research Center."Includes bibliographical references.Mode of access: Inter...

Cold-air performance of compressor-drive turbine of Department of Energy upgraded automobile gas turbine engine /

Roelke, Richard J.
Haas, Jeffrey E.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Propulsion Laboratory (U.S.)
Lewis Research Center.

"October 1982"--Vol. II."Lewis Research Center.""June 1981"--Vol. I."AVRADCOM Research and Technolog...

Cold-air investigation of a 3 1/2-stage fan-drive turbine with a stage loading factor of 4 designed for an integral lift engine /

Whitney, Warren J.
Behning, Frank P.
Schum, Harold J.
Lewis Research Center.

Prepared at Lewis Research Center.Cover title.Includes bibliographical references.1. Turbine design ...

Aerodynamic evaluation of two-stage axial-flow turbine designed for Brayton-cycle space power system /

Kofskey, Milton G.
Nusbaum, William J.
Lewis Research Center.

Prepared at Lewis Research Center."February 1968"--Cover.Includes bibliographical references (p. 28)...

Experimental evaluation of a 3.50-inch radial turbine designed for a 10-kilowatt space power system /

Kofskey, Milton G.
Wasserbauer, Charles A.
United States. National Aeronautics and Space Administration.
Lewis Research Center.

3.50 inch radial turbine designed for 10 kilowatt space power system.Prepared at Lewis Research Cent...

Air-performance evaluation of a 4.0-inch-mean-diameter single-stage turbine at various inlet pressures from 0.14 to 1.88 atmospheres and corresponding Reynolds numbers from 2500 to 50,000 /

Wong, Robert Y.
Nusbaum, William J.
United States. National Aeronautics and Space Administration.

Cover title."August 1962."Power sources, supplementary; Propulsion systems, air-jet.Includes bibliog...

Cold-air investigation of first state of 4 1/2-stage, fan-drive turbine with average stage-loading factor of 4.66 /

Whitney, Warren J.
Behning, Frank P.
Moffitt, Thomas P.
Lewis Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1981

Jan. 1981."Lewis Research Center."Includes bibliographical references.Mode of access: Internet

Experimental investigation of two-stage air-cooled turbine suitable for flight at Mach 2.5 /

Schum, Harold J.
Nunamaker, Robert R.
Petrash, Donald A.
Lewis Research Center.
United States. National Aeronautics and Space Administration.

January 1959

"November 1959."Cover title.Includes bibliographical references (p. 27).Mode of access: Internet

Investigation of two-stage air-cooled turbine suitable for flight at mach number of 2.5.

Miser, James W.
Stewart, Warner L.
Lewis Flight Propulsion Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.
United States. National Advisory Committee for Aeronautics.

January 1956

"October 22, 1956."Includes bibliographical references (p. 17).Mode of access: Internet

Performance of various oxide-magazine cathodes in Kaufman thrusters /

Byers, David C.
Lewis Research Center.

Prepared at Lewis Research Center."March 1969"--Cover.Includes bibliographical references (p. 25-27)...

Performance study of a piston-type pump for liquid hydrogen /

Biermann, Arnold E.
Shinko, William G.
Lewis Research Center.

January 1960

"NASA TN D-276.""Lewis Research Center, Cleveland, Ohio.""March 1960."Cover title.Includes bibliogra...

Steady-state performance of a modified Rankine cycle system using water /

Fenn, David B.
Gutierrez, Orlando A.
Coe, Harold H.
Lewis Research Center.

Prepared at Lewis Research Center."March 1966"--Cover.Includes bibliographical references (p. 18).Mo...

Calculations of the performance of a compression-ignition engine-compressor turbine combination.

Mendelson, Alexander.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Aircraft Engine Research Laboratory.

Prepared at the Aircraft Engine Research Laboratory, Cleveland, Ohio.On front cover: "February 3, 19...

Cold-air performance evaluation of scale model oxidizer pump-drive turbine for the M-1 hydrogen-oxygen rocket engine.

Stabe, Roy G.
Kline, John F.
Lewis Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."February 1968."Includes bibliographical references (p. 19-20).Mode of access: Internet

Research turbine for high-temperature core engine application /

Szanca, Edward M.
Lewis Research Center.

January 1974

Prepared at Lewis Research Center.Cover title.Includes bibliographical references.1. Cold-air overal...

Cold-air investigation of 4 1/2-stage turbine with stage-loading factor of 4.66 and high specific work output : II - stage group performance /

Whitney, Warren J.
Lewis Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1980

"June 1980"--Cover."Lewis Research Center."Includes bibliographical references.Mode of access: Inter...

Cold-air performance of compressor-drive turbine of Department of Energy upgraded automobile gas turbine engine /

Roelke, Richard J.
Haas, Jeffrey E.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Propulsion Laboratory (U.S.)
Lewis Research Center.

"October 1982"--Vol. II."Lewis Research Center.""June 1981"--Vol. I."AVRADCOM Research and Technolog...

Cold-air investigation of a 3 1/2-stage fan-drive turbine with a stage loading factor of 4 designed for an integral lift engine /

Whitney, Warren J.
Behning, Frank P.
Schum, Harold J.
Lewis Research Center.

Prepared at Lewis Research Center.Cover title.Includes bibliographical references.1. Turbine design ...

Aerodynamic evaluation of two-stage axial-flow turbine designed for Brayton-cycle space power system /

Kofskey, Milton G.
Nusbaum, William J.
Lewis Research Center.

Prepared at Lewis Research Center."February 1968"--Cover.Includes bibliographical references (p. 28)...

Experimental evaluation of a 3.50-inch radial turbine designed for a 10-kilowatt space power system /

Kofskey, Milton G.
Wasserbauer, Charles A.
United States. National Aeronautics and Space Administration.
Lewis Research Center.

3.50 inch radial turbine designed for 10 kilowatt space power system.Prepared at Lewis Research Cent...

Air-performance evaluation of a 4.0-inch-mean-diameter single-stage turbine at various inlet pressures from 0.14 to 1.88 atmospheres and corresponding Reynolds numbers from 2500 to 50,000 /

Wong, Robert Y.
Nusbaum, William J.
United States. National Aeronautics and Space Administration.

Cover title."August 1962."Power sources, supplementary; Propulsion systems, air-jet.Includes bibliog...

Cold-air investigation of first state of 4 1/2-stage, fan-drive turbine with average stage-loading factor of 4.66 /

Whitney, Warren J.
Behning, Frank P.
Moffitt, Thomas P.
Lewis Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1981

Jan. 1981."Lewis Research Center."Includes bibliographical references.Mode of access: Internet

Experimental investigation of two-stage air-cooled turbine suitable for flight at Mach 2.5 /

Schum, Harold J.
Nunamaker, Robert R.
Petrash, Donald A.
Lewis Research Center.
United States. National Aeronautics and Space Administration.

January 1959

"November 1959."Cover title.Includes bibliographical references (p. 27).Mode of access: Internet

Investigation of two-stage air-cooled turbine suitable for flight at mach number of 2.5.

Miser, James W.
Stewart, Warner L.
Lewis Flight Propulsion Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.
United States. National Advisory Committee for Aeronautics.

January 1956

"October 22, 1956."Includes bibliographical references (p. 17).Mode of access: Internet

Performance of various oxide-magazine cathodes in Kaufman thrusters /

Byers, David C.
Lewis Research Center.

Prepared at Lewis Research Center."March 1969"--Cover.Includes bibliographical references (p. 25-27)...

Performance study of a piston-type pump for liquid hydrogen /

Biermann, Arnold E.
Shinko, William G.
Lewis Research Center.

January 1960

"NASA TN D-276.""Lewis Research Center, Cleveland, Ohio.""March 1960."Cover title.Includes bibliogra...

Steady-state performance of a modified Rankine cycle system using water /

Fenn, David B.
Gutierrez, Orlando A.
Coe, Harold H.
Lewis Research Center.

Prepared at Lewis Research Center."March 1966"--Cover.Includes bibliographical references (p. 18).Mo...

Calculations of the performance of a compression-ignition engine-compressor turbine combination.

Mendelson, Alexander.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Aircraft Engine Research Laboratory.

Prepared at the Aircraft Engine Research Laboratory, Cleveland, Ohio.On front cover: "February 3, 19...

Cold-air performance evaluation of scale model oxidizer pump-drive turbine for the M-1 hydrogen-oxygen rocket engine.

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Cold-air performance evaluation of scale model oxidizer pump-drive turbine for the M-1 hydrogen-oxygen rocket engine.

Abstract

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