Helium pressurization systems for liquid-methane fuel in supersonic transports /

Combustion of hydrogen injected into a supersonic airstream (the ship computer program) /

Markatos, N. C.
Tatchell, D. G., joint author.
Spalding, D. B. (Dudley Brian), 1923- joint author.
Fluid Mechanics and Thermal Systems.
United States. National Aeronautics and Space Administration.

January 1977

Issued April 1977.Prepared by Fluid Mechanics and Thermal Systems, Inc. for Langley Research Center ...

Exploratory tests of two strut fuel injectors for supersonic combustion /

Anderson, Griffin Y.
Gooderum, Paul B.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 21).Mode of ...

Centrifugal compressor for high-temperature helium : performance characteristics /

Coates, Neil H.
McGee, James P.
Nordlinger, S. G.
U.S. Atomic Energy Commission.
United States. Bureau of Mines.

Work done under cooperative agreement with the U.S. Atomic Energy Commission.Bibliographical referen...

High-energy fuels for supersonic transport reserves /

Eisenberg, Joseph D.
United States. National Aeronautics and Space Administration.
Lewis Research Center.

January 1967

Prepared at Lewis Research Center.Includes bibliographical references (p. 34).Mode of access: Intern...

Comparative study of fuselage tanks for liquid-methane-fueled supersonic aircraft /

Chambellan, Rene E.
Bevevino, William A.
Lewis Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Work performed at Lewis Research Center.N68-36074.Includes bibliographical references (p. 15-16).Mod...

Pressurant requirements for discharge of liquid methane from a 1.52-meter- (5-ft- ) diameter spherical tank under both static and slosh conditions /

DeWitt, Richard L.
McIntire, Thomas O.
Lewis Research Center.

January 1974

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 82-83).Mode of...

Mixing of hydrogen injected from multiple injectors normal to a supersonic airstream /

Rogers, R. Clayton.
United States. National Aeronautics and Space Administration.
Langley Research Center.

January 1971

Prepared at Langley Research Center.N 71-34274.Includes bibliographical references (p. 14-15).Mode o...

Transient performance of a turboalternator gas-bearing system /

Wood, James C.
Asadourian, Armen S.
Curreri, Joseph S.
Lewis Research Center.
United States. National Aeronautics and Space Administration.

January 1970

Experimental operation of gas-bearing turboalternator for spacecraft power supplies.Includes bibliog...

Combustion of hydrogen injected into a supersonic airstream : a guide to the Hiss computer program /

Dyer, David F.
Spalding, D. B. (Dudley Brian), 1923- joint author.
Maples, Glennon.
Fluid Mechanics and Thermal Systems.
United States. National Aeronautics and Space Administration.

January 1976

Prepared by Fluid Mechanics and Thermal Systems, Inc., for Langley Research Center.Cover title.Inclu...

Ideal-gas tables for helium flow in the Mach number range from 40 to 100 /

Mueller, James N.
Langley Research Center.

Prepared at Langley Research Center."May 1962."Cover title.Includes bibliographical references (p. 6...

A study of helium penetration and spreading in a Mach 2 airstream using a delta wing injector /

Povinelli, Louis A.
Hersch, Martin.
Povinelli, Frederick P.
Lewis Research Center.
United States. National Aeronautics and Space Administration.

January 1969

Helium penetration and spreading in Mach 2 airstream using delta wing injector.Includes bibliographi...

Turbulent mixing of coaxial compressible hydrogen-air jets /

Eggers, James M.
United States. National Aeronautics and Space Administration.
Langley Research Center.

January 1971

Prepared at Langley Research Center.N 71-34283.Includes bibliographical references (p. 33-34).Mode o...

Venting characteristics of gaseous helium and nitrogen discharging into a free stream at Mach numbers from 0.60 to 1.57 /

Johns, Albert L.
Jones, Merle L.
Lewis Research Center.

January 1974

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 6).Mode of acc...

Upper stages using liquid propulsion and metallized propellants /

Palaszewski, Bryan A. (Bryan Alan)
Lewis Research Center.

January 1992

Prepared at Lewis Research Center.Includes bibliographical references (p. 18-19).Mode of access: Int...

Gaseous-hydrogen-liquid-oxygen rocket combustion at supercritical chamber pressures /

Hersch, Martin.
Rice, Edward J.
Lewis Research Center.

Prepared at Lewis Research Center."September 1967"--Cover.Includes bibliographical references (p. 18...

Combustion of hydrogen injected into a supersonic airstream (the ship computer program) /

Markatos, N. C.
Tatchell, D. G., joint author.
Spalding, D. B. (Dudley Brian), 1923- joint author.
Fluid Mechanics and Thermal Systems.
United States. National Aeronautics and Space Administration.

January 1977

Issued April 1977.Prepared by Fluid Mechanics and Thermal Systems, Inc. for Langley Research Center ...

Exploratory tests of two strut fuel injectors for supersonic combustion /

Anderson, Griffin Y.
Gooderum, Paul B.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 21).Mode of ...

Centrifugal compressor for high-temperature helium : performance characteristics /

Coates, Neil H.
McGee, James P.
Nordlinger, S. G.
U.S. Atomic Energy Commission.
United States. Bureau of Mines.

Work done under cooperative agreement with the U.S. Atomic Energy Commission.Bibliographical referen...

High-energy fuels for supersonic transport reserves /

Eisenberg, Joseph D.
United States. National Aeronautics and Space Administration.
Lewis Research Center.

January 1967

Prepared at Lewis Research Center.Includes bibliographical references (p. 34).Mode of access: Intern...

Comparative study of fuselage tanks for liquid-methane-fueled supersonic aircraft /

Chambellan, Rene E.
Bevevino, William A.
Lewis Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Work performed at Lewis Research Center.N68-36074.Includes bibliographical references (p. 15-16).Mod...

Pressurant requirements for discharge of liquid methane from a 1.52-meter- (5-ft- ) diameter spherical tank under both static and slosh conditions /

DeWitt, Richard L.
McIntire, Thomas O.
Lewis Research Center.

January 1974

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 82-83).Mode of...

Mixing of hydrogen injected from multiple injectors normal to a supersonic airstream /

Rogers, R. Clayton.
United States. National Aeronautics and Space Administration.
Langley Research Center.

January 1971

Prepared at Langley Research Center.N 71-34274.Includes bibliographical references (p. 14-15).Mode o...

Transient performance of a turboalternator gas-bearing system /

Wood, James C.
Asadourian, Armen S.
Curreri, Joseph S.
Lewis Research Center.
United States. National Aeronautics and Space Administration.

January 1970

Experimental operation of gas-bearing turboalternator for spacecraft power supplies.Includes bibliog...

Combustion of hydrogen injected into a supersonic airstream : a guide to the Hiss computer program /

Dyer, David F.
Spalding, D. B. (Dudley Brian), 1923- joint author.
Maples, Glennon.
Fluid Mechanics and Thermal Systems.
United States. National Aeronautics and Space Administration.

January 1976

Prepared by Fluid Mechanics and Thermal Systems, Inc., for Langley Research Center.Cover title.Inclu...

Ideal-gas tables for helium flow in the Mach number range from 40 to 100 /

Mueller, James N.
Langley Research Center.

Prepared at Langley Research Center."May 1962."Cover title.Includes bibliographical references (p. 6...

A study of helium penetration and spreading in a Mach 2 airstream using a delta wing injector /

Povinelli, Louis A.
Hersch, Martin.
Povinelli, Frederick P.
Lewis Research Center.
United States. National Aeronautics and Space Administration.

January 1969

Helium penetration and spreading in Mach 2 airstream using delta wing injector.Includes bibliographi...

Turbulent mixing of coaxial compressible hydrogen-air jets /

Eggers, James M.
United States. National Aeronautics and Space Administration.
Langley Research Center.

January 1971

Prepared at Langley Research Center.N 71-34283.Includes bibliographical references (p. 33-34).Mode o...

Venting characteristics of gaseous helium and nitrogen discharging into a free stream at Mach numbers from 0.60 to 1.57 /

Johns, Albert L.
Jones, Merle L.
Lewis Research Center.

January 1974

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 6).Mode of acc...

Upper stages using liquid propulsion and metallized propellants /

Palaszewski, Bryan A. (Bryan Alan)
Lewis Research Center.

January 1992

Prepared at Lewis Research Center.Includes bibliographical references (p. 18-19).Mode of access: Int...

Gaseous-hydrogen-liquid-oxygen rocket combustion at supercritical chamber pressures /

Hersch, Martin.
Rice, Edward J.
Lewis Research Center.

Prepared at Lewis Research Center."September 1967"--Cover.Includes bibliographical references (p. 18...

Combustion of hydrogen injected into a supersonic airstream (the ship computer program) /

Markatos, N. C.
Tatchell, D. G., joint author.
Spalding, D. B. (Dudley Brian), 1923- joint author.
Fluid Mechanics and Thermal Systems.
United States. National Aeronautics and Space Administration.

January 1977

Issued April 1977.Prepared by Fluid Mechanics and Thermal Systems, Inc. for Langley Research Center ...

Exploratory tests of two strut fuel injectors for supersonic combustion /

Anderson, Griffin Y.
Gooderum, Paul B.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 21).Mode of ...

Centrifugal compressor for high-temperature helium : performance characteristics /

Coates, Neil H.
McGee, James P.
Nordlinger, S. G.
U.S. Atomic Energy Commission.
United States. Bureau of Mines.

Work done under cooperative agreement with the U.S. Atomic Energy Commission.Bibliographical referen...

Helium pressurization systems for liquid-methane fuel in supersonic transports /

Abstract

Extracted data

Helium pressurization systems for liquid-methane fuel in supersonic transports /

Abstract

Extracted data

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