Design analysis of a subsonic nuclear-powered logistic airplane with helium-cooled reactor /

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...

Aerodynamic characteristics of a canard and an outboard-tail airplane model at high subsonic speeds /

Fournier, Paul G.
United States. National Aeronautics and Space Administration.

Cover title."November 1961."Aerodynamics, aircraft; Aircraft; Stability and control.Includes bibliog...

Analysis of factors affecting selection and design of air-cooled single-stage turbines for turbojet engines

Hubbartt, James E.
Schramm, Wilson B., joint author.
Rossbach, Richard J., joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Lewis Flight Propulsion Laboratory.

On front cover: "September 16, 1954."Title from cover.Includes bibliographical references: p. 24.Mod...

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

Structural concepts for hydrogen-fueled hypersonic airplanes /

Jackson, L. Robert.
Wichorek, Gregory R.
Davis, John G.
United States. National Aeronautics and Space Administration.
Langley Research Center.

"February 1966"--Cover.Includes bibliographical references.Mode of access: Internet

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

Subsonic aerodynamic characteristics of an airplane configuration utilizing a variable-sweep wing having a free-floating apex /

Polhamus, Edward C., 1948-
Hammond, Alexander D.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1965

"July 1965"--Cover.Cover title.Includes bibliographical references (p. 9).Mode of access: Internet

An analysis of VG and VGH operational data from a twin-engine turboprop transport airplane /

Hunter, Paul A.
Walker, Walter G.
United States. National Aeronautics and Space Administration.

Cover title."July 1963."Includes bibliographical references.Mode of access: Internet

Investigation of the subsonic stability and control characteristics of a 1/7-scale model of the North American X-15 airplane with and without fuselage forebody strakes /

Hassell, James L.
Hewes, Donald E.
United States. National Aeronautics and Space Administration.

"February 1960."Cover title.Includes bibliographical references (p. 17).Mode of access: Internet

Wind-tunnel studies at subsonic and transonic speeds of a multiple-mission variable-wing- sweep airplane configuration /

Alford, William J.
Handerson, William P.
Luoma, Arvo A.
Langley Research Center.

January 1959

"November 1959."Cover title.Includes bibliographical references (p. 13).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 a jet condenser for space power /

Platt, Robert J.
Langley Research Center.

Prepared at Langley Research Center."October 1965"--Cover.Includes bibliographical references (p. 15...

Transonic aerodynamic characteristics of a model of a proposed six-engine hull-type seaplane designed for supersonic flight /

Wornom, Dewey E.
United States. National Aeronautics and Space Administration.

"March 1960."Cover title.Includes bibliographical references (p. 9).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 ...

Investigation of low-subsonic flight characteristics of a model of a hypersonic boost-glide configuration having a 78 degree delta wing /by /

Paulson, John W.
Shanks, Robert E.
United States. National Aeronautics and Space Administration.

January 1959

Cover title."October 1959."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...

Aerodynamic characteristics of a canard and an outboard-tail airplane model at high subsonic speeds /

Fournier, Paul G.
United States. National Aeronautics and Space Administration.

Cover title."November 1961."Aerodynamics, aircraft; Aircraft; Stability and control.Includes bibliog...

Analysis of factors affecting selection and design of air-cooled single-stage turbines for turbojet engines

Hubbartt, James E.
Schramm, Wilson B., joint author.
Rossbach, Richard J., joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Lewis Flight Propulsion Laboratory.

On front cover: "September 16, 1954."Title from cover.Includes bibliographical references: p. 24.Mod...

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

Structural concepts for hydrogen-fueled hypersonic airplanes /

Jackson, L. Robert.
Wichorek, Gregory R.
Davis, John G.
United States. National Aeronautics and Space Administration.
Langley Research Center.

"February 1966"--Cover.Includes bibliographical references.Mode of access: Internet

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

Subsonic aerodynamic characteristics of an airplane configuration utilizing a variable-sweep wing having a free-floating apex /

Polhamus, Edward C., 1948-
Hammond, Alexander D.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1965

"July 1965"--Cover.Cover title.Includes bibliographical references (p. 9).Mode of access: Internet

An analysis of VG and VGH operational data from a twin-engine turboprop transport airplane /

Hunter, Paul A.
Walker, Walter G.
United States. National Aeronautics and Space Administration.

Cover title."July 1963."Includes bibliographical references.Mode of access: Internet

Investigation of the subsonic stability and control characteristics of a 1/7-scale model of the North American X-15 airplane with and without fuselage forebody strakes /

Hassell, James L.
Hewes, Donald E.
United States. National Aeronautics and Space Administration.

"February 1960."Cover title.Includes bibliographical references (p. 17).Mode of access: Internet

Wind-tunnel studies at subsonic and transonic speeds of a multiple-mission variable-wing- sweep airplane configuration /

Alford, William J.
Handerson, William P.
Luoma, Arvo A.
Langley Research Center.

January 1959

"November 1959."Cover title.Includes bibliographical references (p. 13).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 a jet condenser for space power /

Platt, Robert J.
Langley Research Center.

Prepared at Langley Research Center."October 1965"--Cover.Includes bibliographical references (p. 15...

Transonic aerodynamic characteristics of a model of a proposed six-engine hull-type seaplane designed for supersonic flight /

Wornom, Dewey E.
United States. National Aeronautics and Space Administration.

"March 1960."Cover title.Includes bibliographical references (p. 9).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 ...

Investigation of low-subsonic flight characteristics of a model of a hypersonic boost-glide configuration having a 78 degree delta wing /by /

Paulson, John W.
Shanks, Robert E.
United States. National Aeronautics and Space Administration.

January 1959

Cover title."October 1959."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...

Aerodynamic characteristics of a canard and an outboard-tail airplane model at high subsonic speeds /

Fournier, Paul G.
United States. National Aeronautics and Space Administration.

Cover title."November 1961."Aerodynamics, aircraft; Aircraft; Stability and control.Includes bibliog...

Analysis of factors affecting selection and design of air-cooled single-stage turbines for turbojet engines

Hubbartt, James E.
Schramm, Wilson B., joint author.
Rossbach, Richard J., joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Lewis Flight Propulsion Laboratory.

On front cover: "September 16, 1954."Title from cover.Includes bibliographical references: p. 24.Mod...

Design analysis of a subsonic nuclear-powered logistic airplane with helium-cooled reactor /

Abstract

Extracted data

Design analysis of a subsonic nuclear-powered logistic airplane with helium-cooled reactor /

Abstract

Extracted data

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