Flightweight radiantly and actively cooled panel : thermal and structural performance /

Thermal design verification testing of the anchored interplanetary monitoring platform "D" /

Medlin, Jere W.
United States. National Aeronautics and Space Administration.

January 1967

Cover title."November 1967."Includes bibliographical references (p. 23).Mode of access: Internet

Design and fabrication of a stringer stiffened discrete tube actively cooled panel for a hypersonic aircraft /

Anthony, Frank M.
Helenbrook, Robert G.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1981

Subject category 39."February 1981."Includes bibliographical references.Mode of access: Internet

An analytical study of heat requirements for icing protection of radomes /

Lewis, James P.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Lewis Flight Propulsion Laboratory.

On front cover: "March 11, 1953."Title from cover.Includes bibliographical references: p. 11.Mode of...

Aerothermal performance of a radiatively and actively cooled panel at Mach 6.6 /

Shore, Charles P.
Weinstein, Irving.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1979

Subject category 34."December 1979"--Cover.Includes bibliographical references.Mode of access: Inter...

A radiant heater to simulate aerodynamic heating in a wind tunnel /

Trussell, Donald H.
Weidman, Deene J. (Deene Jon), 1932-
United States. National Aeronautics and Space Administration.

Cover title."November 1960."Stresses and loads.Includes bibliographical references.Mode of access: I...

Elevated-temperature tests under static and aerodynamic conditions on corrugated-stiffened panels /

Groen, Joseph M.
Rosecrans, Richard.
United States. National Aeronautics and Space Administration.

"September 1959."Cover title.Includes bibliographical references (p. 13).Mode of access: Internet

Elevated-temperature tests under static and aerodynamic conditions on honeycomb-core sandwich panels /

Groen, Joseph M.
Johnson, Aldie E.
United States. National Aeronautics and Space Administration.

"September 1959."Cover title.Includes bibliographical references (p. 14).Mode of access: Internet

Design and testing of a high power spacecraft thermal management system /

McCabe, Michael Edward.
Benner, Steve.
Ku, Jentung.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Division.

January 1988

"June 1988"--Cover.Includes bibliographical references (p. 89).Mode of access: Internet

Development of panel methods for subsonic analysis and design /

Bristow, D. R.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1980

Subject category 02."February 1980"--Cover.Includes bibliographical references.Mode of access: Inter...

1981 current research on aviation weather (bibliography) /

Daniel, Joel.
Frost, Walter, 1935-
George C. Marshall Space Flight Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1982

Subject Category 47."March 1982"--Cover.Includes bibliographies.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

Preliminary results of aerodynamic heating studies on the X-15 airplane /

Banner, Richard D.
Quinn, Robert D.
Kuhl, Albert E.
Flight Research Center (U.S.)

January 1962

"March 1962."Cover title.Includes bibliographical references (p. 12).Mode of access: Internet

Flutter clearance of the horizontal tail of the Bellanca Skyrocket II airplane /

Ricketts, Rodney H.
Farmer, Moses G.
Cazier, F. W.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1982

"September 1982"--Cover.Includes bibliographical references.Mode of access: Internet

Thermal performance and radio-frequency transmissivity of several ablation materials /

Dow, Marvin B.
Croswell, William F.
Pittman, Claud M.
United States. National Aeronautics and Space Administration.

Cover title."November 1964."Includes bibliographical references.Mode of access: Internet

A discussion of methods for reducing aerodynamic heating in supersonic flight /

Eggers, A. J. Jr.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Ames Research Center.

On front cover: "September 1, 1955."Title from cover.Includes bibliographical references (p. 7-10).M...

Thermal design verification testing of the anchored interplanetary monitoring platform "D" /

Medlin, Jere W.
United States. National Aeronautics and Space Administration.

January 1967

Cover title."November 1967."Includes bibliographical references (p. 23).Mode of access: Internet

Design and fabrication of a stringer stiffened discrete tube actively cooled panel for a hypersonic aircraft /

Anthony, Frank M.
Helenbrook, Robert G.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1981

Subject category 39."February 1981."Includes bibliographical references.Mode of access: Internet

An analytical study of heat requirements for icing protection of radomes /

Lewis, James P.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Lewis Flight Propulsion Laboratory.

On front cover: "March 11, 1953."Title from cover.Includes bibliographical references: p. 11.Mode of...

Aerothermal performance of a radiatively and actively cooled panel at Mach 6.6 /

Shore, Charles P.
Weinstein, Irving.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1979

Subject category 34."December 1979"--Cover.Includes bibliographical references.Mode of access: Inter...

A radiant heater to simulate aerodynamic heating in a wind tunnel /

Trussell, Donald H.
Weidman, Deene J. (Deene Jon), 1932-
United States. National Aeronautics and Space Administration.

Cover title."November 1960."Stresses and loads.Includes bibliographical references.Mode of access: I...

Elevated-temperature tests under static and aerodynamic conditions on corrugated-stiffened panels /

Groen, Joseph M.
Rosecrans, Richard.
United States. National Aeronautics and Space Administration.

"September 1959."Cover title.Includes bibliographical references (p. 13).Mode of access: Internet

Elevated-temperature tests under static and aerodynamic conditions on honeycomb-core sandwich panels /

Groen, Joseph M.
Johnson, Aldie E.
United States. National Aeronautics and Space Administration.

"September 1959."Cover title.Includes bibliographical references (p. 14).Mode of access: Internet

Design and testing of a high power spacecraft thermal management system /

McCabe, Michael Edward.
Benner, Steve.
Ku, Jentung.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Division.

January 1988

"June 1988"--Cover.Includes bibliographical references (p. 89).Mode of access: Internet

Development of panel methods for subsonic analysis and design /

Bristow, D. R.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1980

Subject category 02."February 1980"--Cover.Includes bibliographical references.Mode of access: Inter...

1981 current research on aviation weather (bibliography) /

Daniel, Joel.
Frost, Walter, 1935-
George C. Marshall Space Flight Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1982

Subject Category 47."March 1982"--Cover.Includes bibliographies.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

Preliminary results of aerodynamic heating studies on the X-15 airplane /

Banner, Richard D.
Quinn, Robert D.
Kuhl, Albert E.
Flight Research Center (U.S.)

January 1962

"March 1962."Cover title.Includes bibliographical references (p. 12).Mode of access: Internet

Flutter clearance of the horizontal tail of the Bellanca Skyrocket II airplane /

Ricketts, Rodney H.
Farmer, Moses G.
Cazier, F. W.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1982

"September 1982"--Cover.Includes bibliographical references.Mode of access: Internet

Thermal performance and radio-frequency transmissivity of several ablation materials /

Dow, Marvin B.
Croswell, William F.
Pittman, Claud M.
United States. National Aeronautics and Space Administration.

Cover title."November 1964."Includes bibliographical references.Mode of access: Internet

A discussion of methods for reducing aerodynamic heating in supersonic flight /

Eggers, A. J. Jr.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Ames Research Center.

On front cover: "September 1, 1955."Title from cover.Includes bibliographical references (p. 7-10).M...

Thermal design verification testing of the anchored interplanetary monitoring platform "D" /

Medlin, Jere W.
United States. National Aeronautics and Space Administration.

January 1967

Cover title."November 1967."Includes bibliographical references (p. 23).Mode of access: Internet

Design and fabrication of a stringer stiffened discrete tube actively cooled panel for a hypersonic aircraft /

Anthony, Frank M.
Helenbrook, Robert G.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1981

Subject category 39."February 1981."Includes bibliographical references.Mode of access: Internet

An analytical study of heat requirements for icing protection of radomes /

Lewis, James P.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Lewis Flight Propulsion Laboratory.

On front cover: "March 11, 1953."Title from cover.Includes bibliographical references: p. 11.Mode of...

Flightweight radiantly and actively cooled panel : thermal and structural performance /

Abstract

Extracted data

Flightweight radiantly and actively cooled panel : thermal and structural performance /

Abstract

Extracted data

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