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

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)...

Investigations of air-cooled turbine rotors for turbojet engines

Nachtigall, Alfred J.
Ziemer, Robert R., joint author.
Zalabak, Charles F., joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Lewis Flight Propulsion Laboratory.

On front cover: "May 21, 1952."Title from cover.Includes bibliographical references: p. 22.Mode of a...

Analysis and selection of design conditions for a radioisotope brayton-cycle space powerplant /

Klann, John L.
Lewis Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."June 1968."Includes bibliographical references (p. 79-80).Mode of access: Internet

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. 20-21).Mode of access: Internet

Considerations of turbine cooling systems for Mach 3 flight /

Stepka, Francis S.
Lewis Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."April 1968."Includes bibliographical references (p. 32).Mode of access: Internet

Cold-air investigation of prototype Snap-8 turbine

Nusbaum, William J.
Holeski, Donald E.
United States. National Aeronautics and Space Administration.

Cover title."October 1962."Fluid mechanics;Power sources, supplementary; Propulsion system elements;...

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

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...

Design of turbine and experimental performance of first two stages /

Rohlik, Harold E.
Lewis Research Center.

January 1961

"May 1961."Cover title.Includes bibliographical references (p. 16).Mode of access: Internet

Experimental investigation of the partial- admission performance characteristics of a single-stage Mach 2 supersonic turbine /

Moffitt, Thomas P.
Klag, Frederick W.
Langley Research Center.

January 1959

"September 1959."Cover title.Includes bibliographical references (p. 8).Mode of access: Internet

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

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)...

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...

Low-temperature performance of compressed-oxygen closed-circuit breathing apparatus /

Kloos, E. J. (Edwin J.)
Schutz, Robert H.
Beckert, A. J. (Albert J.)
United States. Bureau of Mines.

"October 1968"--Cover.Includes bibliographical references.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)...

Investigations of air-cooled turbine rotors for turbojet engines

Nachtigall, Alfred J.
Ziemer, Robert R., joint author.
Zalabak, Charles F., joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Lewis Flight Propulsion Laboratory.

On front cover: "May 21, 1952."Title from cover.Includes bibliographical references: p. 22.Mode of a...

Analysis and selection of design conditions for a radioisotope brayton-cycle space powerplant /

Klann, John L.
Lewis Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."June 1968."Includes bibliographical references (p. 79-80).Mode of access: Internet

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. 20-21).Mode of access: Internet

Considerations of turbine cooling systems for Mach 3 flight /

Stepka, Francis S.
Lewis Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."April 1968."Includes bibliographical references (p. 32).Mode of access: Internet

Cold-air investigation of prototype Snap-8 turbine

Nusbaum, William J.
Holeski, Donald E.
United States. National Aeronautics and Space Administration.

Cover title."October 1962."Fluid mechanics;Power sources, supplementary; Propulsion system elements;...

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

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...

Design of turbine and experimental performance of first two stages /

Rohlik, Harold E.
Lewis Research Center.

January 1961

"May 1961."Cover title.Includes bibliographical references (p. 16).Mode of access: Internet

Experimental investigation of the partial- admission performance characteristics of a single-stage Mach 2 supersonic turbine /

Moffitt, Thomas P.
Klag, Frederick W.
Langley Research Center.

January 1959

"September 1959."Cover title.Includes bibliographical references (p. 8).Mode of access: Internet

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

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)...

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...

Low-temperature performance of compressed-oxygen closed-circuit breathing apparatus /

Kloos, E. J. (Edwin J.)
Schutz, Robert H.
Beckert, A. J. (Albert J.)
United States. Bureau of Mines.

"October 1968"--Cover.Includes bibliographical references.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)...

Investigations of air-cooled turbine rotors for turbojet engines

Nachtigall, Alfred J.
Ziemer, Robert R., joint author.
Zalabak, Charles F., joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Lewis Flight Propulsion Laboratory.

On front cover: "May 21, 1952."Title from cover.Includes bibliographical references: p. 22.Mode of a...

Analysis and selection of design conditions for a radioisotope brayton-cycle space powerplant /

Klann, John L.
Lewis Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."June 1968."Includes bibliographical references (p. 79-80).Mode of access: Internet

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

Abstract

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

Abstract

Extracted data

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