Demonstration of a sterilizable solid rocket motor system /

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 study for development of aerothermodynamic test model materials and fabrication technique /

Dean, W. G.
Connor, L. E.
Langley Research Center.
Lockheed Missiles and Space Company.

January 1972

"Prepared by Lockheed Missiles & Space Company ... for Langley Research Center."Cover title.Bibliogr...

Impulse and thrust test of a sublimating-solid micropropulsion system /

Forsythe, Richard W.
Goddard Space Flight Center.

Prepared at Goddard Space Flight Center."March 1966"--Cover.Mode of access: Internet

Flight demonstration of a nose-mounted rotating-solid-propellant rocket control system and a comparison with analog studies /

Williams, Kirby H.
James, Robert L., Jr.
Langley Research Center.

Prepared at Langley Research Center."March 1966"--Cover.Includes bibliographical references (p. 20)....

A preliminary investigation of the destruction of solid-propellant rocket motors by impact from small particles /

Carter, David J., Jr.
Langley Research Center.

Prepared at Langley Research Center."September 1960."Cover title.Includes bibliographical references...

Development and demonstration of flueric sounding rocket motor ignition /

Marchese, Vincent P.
Langley Research Center.
Singer Company. Kearfott Division.

"Prepared by the Singer Company, Kearfott Division ... for Langley Research Center.""June 1974."Cove...

Upper-stage space-shuttle propulsion by means of separate scramjet and rocket engines /

Franciscus, Leo C.
Allen, John L.
Lewis Research Center.

January 1972

Prepared at Lewis Research Center.Cover title.Bibliography: p. 46-48.Mode of access: Internet

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...

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 ...

Solid propellant processing factors in rocket motor design.

Horine, Carlton L.
Madison, E.W., joint author.

January 1971

At head of title: NASA space vehicle design criteria (chemical propulsion).Cover title.Bibliography:...

Propulsion fundamentals /

Connors, James F.
Lewis Research Center.

January 1968

"Presented to Lewis Aerospace Explorers, Cleveland, Ohio, 1966-67."Cover title.Includes bibliographi...

A study of the role of pyrotechnic systems on the space shuttle program /

Lake, E. Raymond.
Drexelius, V. W.
Thompson, S. J.
Langley Research Center.
McDonnell Douglas Corporation.

January 1973

"Prepared by McDonnell Douglas Corporation ... for Langley Research Center."Cover title.Includes bib...

Solid propellant selection and characterization.

Scortia, Thomas N., 1926-1986.
Cutforth, Howard G., joint author.

January 1971

At head of title: NASA space vehicle design criteria (chemical propulsion)Cover title.Bibliography: ...

A system for spacecraft attitude control and energy storage /

Shaughnessy, J. D. (John Damian)
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 50-51).Mode ...

Analysis of quasi-hybrid solid rocket booster concepts for advanced earth-to-orbit vehicles /

Zurawski, Robert L.
Rapp, Douglas C.
Lewis Research Center.

January 1987

Prepared at Lewis Research Center."August 1987"--Cover.Includes bibliographical references (p. 23).M...

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 study for development of aerothermodynamic test model materials and fabrication technique /

Dean, W. G.
Connor, L. E.
Langley Research Center.
Lockheed Missiles and Space Company.

January 1972

"Prepared by Lockheed Missiles & Space Company ... for Langley Research Center."Cover title.Bibliogr...

Impulse and thrust test of a sublimating-solid micropropulsion system /

Forsythe, Richard W.
Goddard Space Flight Center.

Prepared at Goddard Space Flight Center."March 1966"--Cover.Mode of access: Internet

Flight demonstration of a nose-mounted rotating-solid-propellant rocket control system and a comparison with analog studies /

Williams, Kirby H.
James, Robert L., Jr.
Langley Research Center.

Prepared at Langley Research Center."March 1966"--Cover.Includes bibliographical references (p. 20)....

A preliminary investigation of the destruction of solid-propellant rocket motors by impact from small particles /

Carter, David J., Jr.
Langley Research Center.

Prepared at Langley Research Center."September 1960."Cover title.Includes bibliographical references...

Development and demonstration of flueric sounding rocket motor ignition /

Marchese, Vincent P.
Langley Research Center.
Singer Company. Kearfott Division.

"Prepared by the Singer Company, Kearfott Division ... for Langley Research Center.""June 1974."Cove...

Upper-stage space-shuttle propulsion by means of separate scramjet and rocket engines /

Franciscus, Leo C.
Allen, John L.
Lewis Research Center.

January 1972

Prepared at Lewis Research Center.Cover title.Bibliography: p. 46-48.Mode of access: Internet

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...

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 ...

Solid propellant processing factors in rocket motor design.

Horine, Carlton L.
Madison, E.W., joint author.

January 1971

At head of title: NASA space vehicle design criteria (chemical propulsion).Cover title.Bibliography:...

Propulsion fundamentals /

Connors, James F.
Lewis Research Center.

January 1968

"Presented to Lewis Aerospace Explorers, Cleveland, Ohio, 1966-67."Cover title.Includes bibliographi...

A study of the role of pyrotechnic systems on the space shuttle program /

Lake, E. Raymond.
Drexelius, V. W.
Thompson, S. J.
Langley Research Center.
McDonnell Douglas Corporation.

January 1973

"Prepared by McDonnell Douglas Corporation ... for Langley Research Center."Cover title.Includes bib...

Solid propellant selection and characterization.

Scortia, Thomas N., 1926-1986.
Cutforth, Howard G., joint author.

January 1971

At head of title: NASA space vehicle design criteria (chemical propulsion)Cover title.Bibliography: ...

A system for spacecraft attitude control and energy storage /

Shaughnessy, J. D. (John Damian)
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 50-51).Mode ...

Analysis of quasi-hybrid solid rocket booster concepts for advanced earth-to-orbit vehicles /

Zurawski, Robert L.
Rapp, Douglas C.
Lewis Research Center.

January 1987

Prepared at Lewis Research Center."August 1987"--Cover.Includes bibliographical references (p. 23).M...

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 study for development of aerothermodynamic test model materials and fabrication technique /

Dean, W. G.
Connor, L. E.
Langley Research Center.
Lockheed Missiles and Space Company.

January 1972

"Prepared by Lockheed Missiles & Space Company ... for Langley Research Center."Cover title.Bibliogr...

Impulse and thrust test of a sublimating-solid micropropulsion system /

Forsythe, Richard W.
Goddard Space Flight Center.

Prepared at Goddard Space Flight Center."March 1966"--Cover.Mode of access: Internet

Demonstration of a sterilizable solid rocket motor system /

Abstract

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Demonstration of a sterilizable solid rocket motor system /

Abstract

Extracted data

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