Effect of aerodynamic and angle-of-attack uncertainties on the blended entry flight control system of the space shuttle from Mach 10 to 2.5 /

Effect of aerodynamic and angle-of-attack uncertainties on the May 1979 entry flight control system of the Space Shuttle from Mach 8 to 1.5

Stone, H. W.
Powell, R. W.

January 1985

A six degree of freedom simulation analysis was performed for the space shuttle orbiter during entry...

The lateral and directional aerodynamic characteristics of a re-entry configuration based on a blunt 13° half cone at Mach numbers to 0.90 /

Kenyon, George C.
Ames Research Center.

January 1961

"November 1961."Cover title.Includes bibliographical references (p. 10).Mode of access: Internet

Calculation of aerodynamic characteristics of airplane configurations at high angles of attack /

Tseng, Jing-Biau.
Lan, C. Edward (Chun-Tau Edward), 1935-
Langley Research Center.

January 1988

"October 1988"--Cover."Prepared for Langley Research Center under Grant NAG1-635."Includes bibliogra...

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)...

Simulator evaluation of the effects of reduced spoiler and thrust authority on a decoupled longitudinal control system during landings in wind shear /

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

January 1981

Subject Category 08."October 1981"--Cover."Langley Research Center."Includes bibliographical referen...

Interference effects of canard controls on the longitudinal aerodynamic characteristics of a winged body at Mach 10 /

Brooks, Cuyler W.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."April 1968."Includes bibliographical references (p. 11).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...

Effect of longitudinal and lateral controls on winged reentry configuration at mach 1.97 and angles of attack up to 90° /

Foster, Gerald V.
United States. National Aeronautics and Space Administration.

January 1961

"February 1961."Includes bibliographical references (p. 5).Mode of access: Internet

Control of the space shuttle angle-of-attack during reentry

Ganji, Farid, 1967-

January 2002

Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Mechanical Engineering, 2002.Includes...

Steady internal flow and aerodynamic loads analysis of shuttle thermal protection system /

Petley, D. H.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1984

Subject category 18."March 1984"--Cover.Distributed to depository libraries in microfiche.Includes b...

Effect of modifications on aerodynamic characteristics of a single-stage-to-orbit vehicle at Mach 5.9 /

Bernot, Peter T.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

"January 1983"--Cover."Langley Research Center."Includes bibliographical references.Mode of access: ...

Aerodynamic interactions from reaction controls for lateral control of the M2-F2 lifting-body entry configuration at transonic and supersonic mach numbers /

Bailey, Rodney O.
Brownson, Jack J.
Ames Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1979

Subject category 02."November 1979"--Cover."Ames Research Center."Includes bibliographical reference...

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 ...

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...

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 ...

Effect of aerodynamic and angle-of-attack uncertainties on the May 1979 entry flight control system of the Space Shuttle from Mach 8 to 1.5

Stone, H. W.
Powell, R. W.

January 1985

A six degree of freedom simulation analysis was performed for the space shuttle orbiter during entry...

The lateral and directional aerodynamic characteristics of a re-entry configuration based on a blunt 13° half cone at Mach numbers to 0.90 /

Kenyon, George C.
Ames Research Center.

January 1961

"November 1961."Cover title.Includes bibliographical references (p. 10).Mode of access: Internet

Calculation of aerodynamic characteristics of airplane configurations at high angles of attack /

Tseng, Jing-Biau.
Lan, C. Edward (Chun-Tau Edward), 1935-
Langley Research Center.

January 1988

"October 1988"--Cover."Prepared for Langley Research Center under Grant NAG1-635."Includes bibliogra...

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)...

Simulator evaluation of the effects of reduced spoiler and thrust authority on a decoupled longitudinal control system during landings in wind shear /

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

January 1981

Subject Category 08."October 1981"--Cover."Langley Research Center."Includes bibliographical referen...

Interference effects of canard controls on the longitudinal aerodynamic characteristics of a winged body at Mach 10 /

Brooks, Cuyler W.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."April 1968."Includes bibliographical references (p. 11).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...

Effect of longitudinal and lateral controls on winged reentry configuration at mach 1.97 and angles of attack up to 90° /

Foster, Gerald V.
United States. National Aeronautics and Space Administration.

January 1961

"February 1961."Includes bibliographical references (p. 5).Mode of access: Internet

Control of the space shuttle angle-of-attack during reentry

Ganji, Farid, 1967-

January 2002

Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Mechanical Engineering, 2002.Includes...

Steady internal flow and aerodynamic loads analysis of shuttle thermal protection system /

Petley, D. H.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1984

Subject category 18."March 1984"--Cover.Distributed to depository libraries in microfiche.Includes b...

Effect of modifications on aerodynamic characteristics of a single-stage-to-orbit vehicle at Mach 5.9 /

Bernot, Peter T.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

"January 1983"--Cover."Langley Research Center."Includes bibliographical references.Mode of access: ...

Aerodynamic interactions from reaction controls for lateral control of the M2-F2 lifting-body entry configuration at transonic and supersonic mach numbers /

Bailey, Rodney O.
Brownson, Jack J.
Ames Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1979

Subject category 02."November 1979"--Cover."Ames Research Center."Includes bibliographical reference...

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 ...

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...

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 ...

Effect of aerodynamic and angle-of-attack uncertainties on the May 1979 entry flight control system of the Space Shuttle from Mach 8 to 1.5

Stone, H. W.
Powell, R. W.

January 1985

A six degree of freedom simulation analysis was performed for the space shuttle orbiter during entry...

The lateral and directional aerodynamic characteristics of a re-entry configuration based on a blunt 13° half cone at Mach numbers to 0.90 /

Kenyon, George C.
Ames Research Center.

January 1961

"November 1961."Cover title.Includes bibliographical references (p. 10).Mode of access: Internet

Calculation of aerodynamic characteristics of airplane configurations at high angles of attack /

Tseng, Jing-Biau.
Lan, C. Edward (Chun-Tau Edward), 1935-
Langley Research Center.

January 1988

"October 1988"--Cover."Prepared for Langley Research Center under Grant NAG1-635."Includes bibliogra...

Effect of aerodynamic and angle-of-attack uncertainties on the blended entry flight control system of the space shuttle from Mach 10 to 2.5 /

Abstract

Extracted data

Effect of aerodynamic and angle-of-attack uncertainties on the blended entry flight control system of the space shuttle from Mach 10 to 2.5 /

Abstract

Extracted data

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