A high-performance 250-pound-thrust rocket engine utilizing coaxial-flow injection of JP-4 fuel and liquid oxygen /

Design and evaluation of an oxidant-fuel-ratio-zoned rocket injector for high performance and ablative engine compatibility /

Winter, Jerry M.
Shinn, Arthur M.
Pavli, Albert J.
Lewis Research Center.

January 1972

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 28).Mode of ac...

A combined water-bromotrifluoromethane crash-fire protection system for a T-56 turbopropeller engine /

Campbell, John A.
Busch, Arthur M.
Lewis Research Center.

January 1959

"NASA TN D-28.""Lewis Research Center, Cleveland, Ohio""August 1959."Title from cover.Includes bibli...

Flight test performance and description of a rocket vehicle for producing low-speed artificial meteors /

Brown, Clarence A.
Keating, Jean C.
Langley Research Center.

Prepared at Langley Research Center."April 1964"--Cover.Includes bibliographical references (p. 9).M...

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...

Control of combustion-chamber pressure and oxidant-fuel ratio for a regeneratively cooled hydrogen-fluorine rocket engine /

Otto, Edward W.
Flage, Richard A.
Lewis Research Center.

January 1959

"NASA TN D-82.""Lewis Research Center, Cleveland, Ohio.""November 1959."Title from cover.Includes bi...

Base flow characteristics for several four-clustered rocket configurations at mach numbers from 2.0 to 3.5 /

Musial, Normal T.
Ward, James J.
United States. National Aeronautics and Space Administration.

Cover title."December 1961."Aerodynamics, missiles and space vehicles; Propulsion systems, liquid-fu...

Investigation of injectors for a low-chamber-pressure hydrogen-fluorine rocket engine /

Price, Harold G.
Shinn, Arthur M.
Lubick, Robert J.
Lewis Research Center.

January 1962

"July 1962."Cover title.Includes bibliographical references (p. 10-11).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...

Orbital investigation of propellant dynamics in a large rocket booster /

Buchanan, H.J.
Bugg, F.M.
George C. Marshall Space Flight Center.
United States. National Aeronautics and Space Administration.

January 1967

Cover title."May 1967."Includes bibliographical references (p. 16).Mode of access: Internet

Performance of a low-thrust storable propellant rocket at very low chamber pressure /

Wanhainen, John P.
Ross, Phil S.
DeWitt, Richard L.
United States. National Aeronautics and Space Administration.

Cover title."March 1961."Propulsion system elements; Propulsion systems, liquid-fuel rockets; Stab...

Flight performance of a spin-stabilized 20-inch-diameter solid-propellant spherical rocket motor/

United States. National Aeronautics and Space Administration.

Cover title." September 1960."Major NASA subject terms:Includes bibliographical references.Mode of a...

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

Control of a large launch vehicle with limited thrust vectoring in the presence of winds /

Collins, Dennis F. (Dennis Francis), 1936-
Morgan, Homer G.
Langley Research Center.

Prepared at Langley Research Center."August 1963."Cover title.Includes bibliographical references (p...

Experimental thrust performance of a high-area-ratio rocket nozzle /

Pavli, Albert J.
Smith, Tamara A.
Kacynski, Kenneth J.
Lewis Research Center.

January 1987

Prepared at Lewis Research Center."April 1987"--Cover.Includes bibliographical references (p. 13).Mo...

Experimental investigation in an altitude test facility of burning of excess combustibles in a rocket engine exhaust /

Bloomer, Harry E.
Antl, Robert J.
Renas, Paul E.
Lewis Research Center.

January 1960

"NASA TN D-200.""Lewis Research Center, Cleveland, Ohio.""January 1960."Title from cover.Includes bi...

Design and evaluation of an oxidant-fuel-ratio-zoned rocket injector for high performance and ablative engine compatibility /

Winter, Jerry M.
Shinn, Arthur M.
Pavli, Albert J.
Lewis Research Center.

January 1972

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 28).Mode of ac...

A combined water-bromotrifluoromethane crash-fire protection system for a T-56 turbopropeller engine /

Campbell, John A.
Busch, Arthur M.
Lewis Research Center.

January 1959

"NASA TN D-28.""Lewis Research Center, Cleveland, Ohio""August 1959."Title from cover.Includes bibli...

Flight test performance and description of a rocket vehicle for producing low-speed artificial meteors /

Brown, Clarence A.
Keating, Jean C.
Langley Research Center.

Prepared at Langley Research Center."April 1964"--Cover.Includes bibliographical references (p. 9).M...

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...

Control of combustion-chamber pressure and oxidant-fuel ratio for a regeneratively cooled hydrogen-fluorine rocket engine /

Otto, Edward W.
Flage, Richard A.
Lewis Research Center.

January 1959

"NASA TN D-82.""Lewis Research Center, Cleveland, Ohio.""November 1959."Title from cover.Includes bi...

Base flow characteristics for several four-clustered rocket configurations at mach numbers from 2.0 to 3.5 /

Musial, Normal T.
Ward, James J.
United States. National Aeronautics and Space Administration.

Cover title."December 1961."Aerodynamics, missiles and space vehicles; Propulsion systems, liquid-fu...

Investigation of injectors for a low-chamber-pressure hydrogen-fluorine rocket engine /

Price, Harold G.
Shinn, Arthur M.
Lubick, Robert J.
Lewis Research Center.

January 1962

"July 1962."Cover title.Includes bibliographical references (p. 10-11).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...

Orbital investigation of propellant dynamics in a large rocket booster /

Buchanan, H.J.
Bugg, F.M.
George C. Marshall Space Flight Center.
United States. National Aeronautics and Space Administration.

January 1967

Cover title."May 1967."Includes bibliographical references (p. 16).Mode of access: Internet

Performance of a low-thrust storable propellant rocket at very low chamber pressure /

Wanhainen, John P.
Ross, Phil S.
DeWitt, Richard L.
United States. National Aeronautics and Space Administration.

Cover title."March 1961."Propulsion system elements; Propulsion systems, liquid-fuel rockets; Stab...

Flight performance of a spin-stabilized 20-inch-diameter solid-propellant spherical rocket motor/

United States. National Aeronautics and Space Administration.

Cover title." September 1960."Major NASA subject terms:Includes bibliographical references.Mode of a...

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

Control of a large launch vehicle with limited thrust vectoring in the presence of winds /

Collins, Dennis F. (Dennis Francis), 1936-
Morgan, Homer G.
Langley Research Center.

Prepared at Langley Research Center."August 1963."Cover title.Includes bibliographical references (p...

Experimental thrust performance of a high-area-ratio rocket nozzle /

Pavli, Albert J.
Smith, Tamara A.
Kacynski, Kenneth J.
Lewis Research Center.

January 1987

Prepared at Lewis Research Center."April 1987"--Cover.Includes bibliographical references (p. 13).Mo...

Experimental investigation in an altitude test facility of burning of excess combustibles in a rocket engine exhaust /

Bloomer, Harry E.
Antl, Robert J.
Renas, Paul E.
Lewis Research Center.

January 1960

"NASA TN D-200.""Lewis Research Center, Cleveland, Ohio.""January 1960."Title from cover.Includes bi...

Design and evaluation of an oxidant-fuel-ratio-zoned rocket injector for high performance and ablative engine compatibility /

Winter, Jerry M.
Shinn, Arthur M.
Pavli, Albert J.
Lewis Research Center.

January 1972

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 28).Mode of ac...

A combined water-bromotrifluoromethane crash-fire protection system for a T-56 turbopropeller engine /

Campbell, John A.
Busch, Arthur M.
Lewis Research Center.

January 1959

"NASA TN D-28.""Lewis Research Center, Cleveland, Ohio""August 1959."Title from cover.Includes bibli...

Flight test performance and description of a rocket vehicle for producing low-speed artificial meteors /

Brown, Clarence A.
Keating, Jean C.
Langley Research Center.

Prepared at Langley Research Center."April 1964"--Cover.Includes bibliographical references (p. 9).M...

A high-performance 250-pound-thrust rocket engine utilizing coaxial-flow injection of JP-4 fuel and liquid oxygen /

Abstract

Extracted data

A high-performance 250-pound-thrust rocket engine utilizing coaxial-flow injection of JP-4 fuel and liquid oxygen /

Abstract

Extracted data

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