High-temperature dielectric properties of candidate space-shuttle thermal-protection-system and antenna-window materials /

Subsonic and transonic dynamic-stability characteristics of the space shuttle launch vehicle /

Freeman, Delma C.
Davenport, Edwin E., joint author.
Boyden, Richmond P., joint author.
Langley Research Center.

January 1976

Cover title.Includes bibliographical references (p. 11).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

Subsonic and transonic dynamic stability characteristics of a space shuttle orbiter /

Boyden, Richmond P.
Freeman, Delma C.
Langley Research Center.

January 1975

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

Investigation of high temperature antennas for space shuttle /

Kuhlman, E. A.
Langley Research Center.
McDonnell Douglas Astronautics Company-East.

January 1973

"Prepared by McDonnell Douglas Astronautics Company-East ... for Langley Research Center."Cover titl...

Aperture excited dielectric antennas /

Croswell, W. F.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 49).Mode of ...

Ablative heat shield design for space shuttle /

Seiferth, Rolf W.
Langley Research Center.
Martin Marietta Denver Aerospace.

January 1975

"Prepared by Martin Marietta Corporation, Denver, Colo. ... for Langley Research Center."Cover title...

Measured catalycities of various candidate space shuttle thermal protection system coatings at low temperatures /

Scott, Carl D.
Manned Spacecraft Center (U.S.)

January 1973

Prepared at the Manned Spacecraft Center, Houston, Tex.Cover title.Bibliography: p. 21.Mode of acces...

High-power-level temperature controller for space flight applications /

Harrigill, William T.
Smith, L. Jack.
Lewis Research Center.

Prepared at Lewis Research Center."March 1966"--Cover.Includes bibliographical references (p. 15).Mo...

Studies relating to temperature control of a large space telescope /

Katzoff, S. (Samuel), 1909-
Langley Research Center.

January 1973

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 41-42).Mode ...

Complex permittivity measurements during high temperature recycling of space shuttle antenna windows and dielectric heat shield materials

Bomar, Steve Herren

January 1972

Issued as Monthly technical letter progress report, no. 1-13/14, and Final report, Project no. A-138

Dielectric measurements on high-temperature materials

Westphal, W. B.
Iglesias, J.
Massachusetts Institute of Technology. Laboratory for Insulation Research.

January 1970

Prepared by Massachusetts Institute of Technology, Laboratory for Insulation Research, under USAF Co...

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...

Influence of configuration details on the subsonic characteristics of a space shuttle orbiter design /

Decker, John P.
Phillips, W. Pelham.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 9).Mode of a...

Supersonic dynamic stability characteristics of a space shuttle orbiter /

Freeman, Delma C.
Davenport, Edwin E.
Boyden, Richmond P.
Langley Research Center.

January 1976

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 25).Mode of ...

Radiative properties of advanced spacecraft heat shield materials /

Cunnington, G. R.
Funai, A. I.
McNab, T. K.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Lockheed Missiles and Space Company.

January 1983

"Lockheed Missiles and Space Company, Inc."Subject category 26."November 1983"--Cover.Distributed to...

Subsonic and transonic dynamic-stability characteristics of the space shuttle launch vehicle /

Freeman, Delma C.
Davenport, Edwin E., joint author.
Boyden, Richmond P., joint author.
Langley Research Center.

January 1976

Cover title.Includes bibliographical references (p. 11).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

Subsonic and transonic dynamic stability characteristics of a space shuttle orbiter /

Boyden, Richmond P.
Freeman, Delma C.
Langley Research Center.

January 1975

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

Investigation of high temperature antennas for space shuttle /

Kuhlman, E. A.
Langley Research Center.
McDonnell Douglas Astronautics Company-East.

January 1973

"Prepared by McDonnell Douglas Astronautics Company-East ... for Langley Research Center."Cover titl...

Aperture excited dielectric antennas /

Croswell, W. F.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 49).Mode of ...

Ablative heat shield design for space shuttle /

Seiferth, Rolf W.
Langley Research Center.
Martin Marietta Denver Aerospace.

January 1975

"Prepared by Martin Marietta Corporation, Denver, Colo. ... for Langley Research Center."Cover title...

Measured catalycities of various candidate space shuttle thermal protection system coatings at low temperatures /

Scott, Carl D.
Manned Spacecraft Center (U.S.)

January 1973

Prepared at the Manned Spacecraft Center, Houston, Tex.Cover title.Bibliography: p. 21.Mode of acces...

High-power-level temperature controller for space flight applications /

Harrigill, William T.
Smith, L. Jack.
Lewis Research Center.

Prepared at Lewis Research Center."March 1966"--Cover.Includes bibliographical references (p. 15).Mo...

Studies relating to temperature control of a large space telescope /

Katzoff, S. (Samuel), 1909-
Langley Research Center.

January 1973

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 41-42).Mode ...

Complex permittivity measurements during high temperature recycling of space shuttle antenna windows and dielectric heat shield materials

Bomar, Steve Herren

January 1972

Issued as Monthly technical letter progress report, no. 1-13/14, and Final report, Project no. A-138

Dielectric measurements on high-temperature materials

Westphal, W. B.
Iglesias, J.
Massachusetts Institute of Technology. Laboratory for Insulation Research.

January 1970

Prepared by Massachusetts Institute of Technology, Laboratory for Insulation Research, under USAF Co...

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...

Influence of configuration details on the subsonic characteristics of a space shuttle orbiter design /

Decker, John P.
Phillips, W. Pelham.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 9).Mode of a...

Supersonic dynamic stability characteristics of a space shuttle orbiter /

Freeman, Delma C.
Davenport, Edwin E.
Boyden, Richmond P.
Langley Research Center.

January 1976

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 25).Mode of ...

Radiative properties of advanced spacecraft heat shield materials /

Cunnington, G. R.
Funai, A. I.
McNab, T. K.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Lockheed Missiles and Space Company.

January 1983

"Lockheed Missiles and Space Company, Inc."Subject category 26."November 1983"--Cover.Distributed to...

Subsonic and transonic dynamic-stability characteristics of the space shuttle launch vehicle /

Freeman, Delma C.
Davenport, Edwin E., joint author.
Boyden, Richmond P., joint author.
Langley Research Center.

January 1976

Cover title.Includes bibliographical references (p. 11).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

Subsonic and transonic dynamic stability characteristics of a space shuttle orbiter /

Boyden, Richmond P.
Freeman, Delma C.
Langley Research Center.

January 1975

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

High-temperature dielectric properties of candidate space-shuttle thermal-protection-system and antenna-window materials /

Abstract

Extracted data

High-temperature dielectric properties of candidate space-shuttle thermal-protection-system and antenna-window materials /

Abstract

Extracted data

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