Wind-tunnel roll-damping measurements of a winged space shuttle configuration in launch attitude /

Influence of orbital-maneuvering-system fairings and rudder flare on the transonic aerodynamic characteristics of a space shuttle orbiter /

Ellison, James C. (James Charles), 1939-
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 8).Mode of a...

Analysis of wing-body interaction flutter for a preliminary space shuttle design /

Chipman, Richard R.
Shyprykevich, Peter.
Langley Research Center.
Grumman Aerospace Corporation.

January 1974

Errata sheet inserted."Prepared by Grumman Aerospace Corporation ... for Langley Research Center."Co...

Grumman H-33 space shuttle orbiter aerodynamic and handling-qualities study /

Rainey, Robert W. (Robert Weaver), 1921-
Langley Research Center.

January 1972

Prepared at Langley Research Center.Cover title.Bibliography: p. 11.Mode of access: Internet

Subsonic roll-damping characteristics of a series of wings /

Boyden, Richmond P.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 10-11).Mode ...

Aerodynamic roll damping of a T-tail transport configuration /

Boyden, Richmond P.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 12).Mode of ...

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 ...

Supersonic dynamic-stability derivatives of the space shuttle launch vehicle /

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

January 1976

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 11).Mode of ...

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

Aerodynamic characteristics of a large aircraft to transport space shuttle orbiter or other external payloads /

Paulson, John W.
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 12).Mode of ...

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...

Dynamic stability derivatives of space shuttle orbiter from wind-tunnel and approach and landing flight tests /

Freeman, Delma C.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1980

"Langley Research Center.""April 1980"--Cover.Includes bibliographical references.Mode of access: In...

Analytical and experimental vibration studies of a 1/8 scale shuttle orbiter /

Pinson, Larry D.
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 69-71).Mode ...

Computer-aided space shuttle orbiter wing design study /

Phillips, W. Pelham.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 84).Mode of ...

An in-flight technique for wind measurement in support of the space shuttle program /

Bjarke, Lisa J.
Ehernberger, L. J.
Dryden Flight Research Facility.

January 1989

Research performed at Dryden Flight Research Facility.Bibliography: p. 6.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

Influence of orbital-maneuvering-system fairings and rudder flare on the transonic aerodynamic characteristics of a space shuttle orbiter /

Ellison, James C. (James Charles), 1939-
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 8).Mode of a...

Analysis of wing-body interaction flutter for a preliminary space shuttle design /

Chipman, Richard R.
Shyprykevich, Peter.
Langley Research Center.
Grumman Aerospace Corporation.

January 1974

Errata sheet inserted."Prepared by Grumman Aerospace Corporation ... for Langley Research Center."Co...

Grumman H-33 space shuttle orbiter aerodynamic and handling-qualities study /

Rainey, Robert W. (Robert Weaver), 1921-
Langley Research Center.

January 1972

Prepared at Langley Research Center.Cover title.Bibliography: p. 11.Mode of access: Internet

Subsonic roll-damping characteristics of a series of wings /

Boyden, Richmond P.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 10-11).Mode ...

Aerodynamic roll damping of a T-tail transport configuration /

Boyden, Richmond P.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 12).Mode of ...

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 ...

Supersonic dynamic-stability derivatives of the space shuttle launch vehicle /

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

January 1976

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 11).Mode of ...

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

Aerodynamic characteristics of a large aircraft to transport space shuttle orbiter or other external payloads /

Paulson, John W.
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 12).Mode of ...

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...

Dynamic stability derivatives of space shuttle orbiter from wind-tunnel and approach and landing flight tests /

Freeman, Delma C.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1980

"Langley Research Center.""April 1980"--Cover.Includes bibliographical references.Mode of access: In...

Analytical and experimental vibration studies of a 1/8 scale shuttle orbiter /

Pinson, Larry D.
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 69-71).Mode ...

Computer-aided space shuttle orbiter wing design study /

Phillips, W. Pelham.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 84).Mode of ...

An in-flight technique for wind measurement in support of the space shuttle program /

Bjarke, Lisa J.
Ehernberger, L. J.
Dryden Flight Research Facility.

January 1989

Research performed at Dryden Flight Research Facility.Bibliography: p. 6.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

Influence of orbital-maneuvering-system fairings and rudder flare on the transonic aerodynamic characteristics of a space shuttle orbiter /

Ellison, James C. (James Charles), 1939-
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 8).Mode of a...

Analysis of wing-body interaction flutter for a preliminary space shuttle design /

Chipman, Richard R.
Shyprykevich, Peter.
Langley Research Center.
Grumman Aerospace Corporation.

January 1974

Errata sheet inserted."Prepared by Grumman Aerospace Corporation ... for Langley Research Center."Co...

Grumman H-33 space shuttle orbiter aerodynamic and handling-qualities study /

Rainey, Robert W. (Robert Weaver), 1921-
Langley Research Center.

January 1972

Prepared at Langley Research Center.Cover title.Bibliography: p. 11.Mode of access: Internet

Wind-tunnel roll-damping measurements of a winged space shuttle configuration in launch attitude /

Abstract

Extracted data

Wind-tunnel roll-damping measurements of a winged space shuttle configuration in launch attitude /

Abstract

Extracted data

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