Comparison of space shuttle orbiter low-speed static stability and control derivatives obtained from wind-tunnel and approach and landing flight tests /

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...

Flight performance of a navigation, guidance, and control system concept for automatic approach and landing of the space shuttle orbiter /

Edwards, Frederick G.
Ames Research Center.

January 1975

Prepared at Ames Research Center.Cover title.Includes bibliographical references (p. 29).Mode of acc...

Force and moment flow-visualization, and boundary-layer tests on a Shuttle Orbiter model at Mach 6 /

Calloway, Robert L.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Langley Research Center.

January 1981

Subject Category 02."Langley Research Center.""December 1981"--Cover.Includes bibliographical refere...

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...

Analysis of the space shuttle orbiter entry dynamics from Mach 10 to Mach 2.5 with the November 1976 flight control system /

Powell, Richard W.
Stone, Howard W.
Langley Research Center.

January 1980

Prepared at Langley Research Center."August 1980"--Cover.Includes bibliographical references (p. 33)...

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 ...

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

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 ...

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

Hess, R. W. (Robert W.)
Davenport, Edwin E.
Langley Research Center.

January 1973

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

Development of the reentry flight dynamics simulator for evaluation of space shuttle orbiter entry systems /

Rowell, Lawrence F.
Stone, Howard W.
Powell, Richard W.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1980

"Oct. 1980."Langley Research Center."Includes bibliographical references.Mode of access: Internet

Comparison of analytical and wind-tunnel results for flutter and gust response of a transport wing with active controls /

Abel, Irving.
Newsom, Jerry R.
Perry, Boyd.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Langley Research Center.

January 1982

Subject category 39."June 1982"--Cover."Langley Research Center."Includes bibliographical references...

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 ...

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

Comparison of analytical predictions of longitudinal short-period pilot-induced oscillations with results from a simulation study of the space shuttle orbiter /

Riley, Donald R.
Miller, G. Kimball.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Langley Research Center.

January 1982

"April 1982"--Cover."Langley Research Center."Includes bibliographical references.Mode of access: In...

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...

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...

Flight performance of a navigation, guidance, and control system concept for automatic approach and landing of the space shuttle orbiter /

Edwards, Frederick G.
Ames Research Center.

January 1975

Prepared at Ames Research Center.Cover title.Includes bibliographical references (p. 29).Mode of acc...

Force and moment flow-visualization, and boundary-layer tests on a Shuttle Orbiter model at Mach 6 /

Calloway, Robert L.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Langley Research Center.

January 1981

Subject Category 02."Langley Research Center.""December 1981"--Cover.Includes bibliographical refere...

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...

Analysis of the space shuttle orbiter entry dynamics from Mach 10 to Mach 2.5 with the November 1976 flight control system /

Powell, Richard W.
Stone, Howard W.
Langley Research Center.

January 1980

Prepared at Langley Research Center."August 1980"--Cover.Includes bibliographical references (p. 33)...

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 ...

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

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 ...

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

Hess, R. W. (Robert W.)
Davenport, Edwin E.
Langley Research Center.

January 1973

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

Development of the reentry flight dynamics simulator for evaluation of space shuttle orbiter entry systems /

Rowell, Lawrence F.
Stone, Howard W.
Powell, Richard W.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1980

"Oct. 1980."Langley Research Center."Includes bibliographical references.Mode of access: Internet

Comparison of analytical and wind-tunnel results for flutter and gust response of a transport wing with active controls /

Abel, Irving.
Newsom, Jerry R.
Perry, Boyd.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Langley Research Center.

January 1982

Subject category 39."June 1982"--Cover."Langley Research Center."Includes bibliographical references...

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 ...

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

Comparison of analytical predictions of longitudinal short-period pilot-induced oscillations with results from a simulation study of the space shuttle orbiter /

Riley, Donald R.
Miller, G. Kimball.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Langley Research Center.

January 1982

"April 1982"--Cover."Langley Research Center."Includes bibliographical references.Mode of access: In...

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...

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...

Flight performance of a navigation, guidance, and control system concept for automatic approach and landing of the space shuttle orbiter /

Edwards, Frederick G.
Ames Research Center.

January 1975

Prepared at Ames Research Center.Cover title.Includes bibliographical references (p. 29).Mode of acc...

Force and moment flow-visualization, and boundary-layer tests on a Shuttle Orbiter model at Mach 6 /

Calloway, Robert L.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Langley Research Center.

January 1981

Subject Category 02."Langley Research Center.""December 1981"--Cover.Includes bibliographical refere...

Comparison of space shuttle orbiter low-speed static stability and control derivatives obtained from wind-tunnel and approach and landing flight tests /

Abstract

Extracted data

Comparison of space shuttle orbiter low-speed static stability and control derivatives obtained from wind-tunnel and approach and landing flight tests /

Abstract

Extracted data

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