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

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 ...

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...

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...

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

Freeman, Delma C.
Spencer, Bernard, 1932-
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1980

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

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 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

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)...

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

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...

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 ...

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

Dynamic model investigation of touchdown stability of lunar-landing vehicles /

Herr, Robert W.
Leonard, H. Wayne.
Langley Research Center.

Prepared at Langley Research Center."October 1967"--Cover.Includes bibliographical references (p. 22...

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...

Sensitivity analysis of the space shuttle to ascent wind profiles /

Smith, Orvel E.
Austin, Lambert D.
Lyndon B. Johnson Space Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
George C. Marshall Space Flight Center.

January 1982

"George C. Marshall Space Flight Center.""March 1982"--Cover."Lyndon B. Johnson Space Center."Includ...

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 ...

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...

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...

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

Freeman, Delma C.
Spencer, Bernard, 1932-
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1980

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

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 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

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)...

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

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...

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 ...

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

Dynamic model investigation of touchdown stability of lunar-landing vehicles /

Herr, Robert W.
Leonard, H. Wayne.
Langley Research Center.

Prepared at Langley Research Center."October 1967"--Cover.Includes bibliographical references (p. 22...

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...

Sensitivity analysis of the space shuttle to ascent wind profiles /

Smith, Orvel E.
Austin, Lambert D.
Lyndon B. Johnson Space Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
George C. Marshall Space Flight Center.

January 1982

"George C. Marshall Space Flight Center.""March 1982"--Cover."Lyndon B. Johnson Space Center."Includ...

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 ...

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...

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...

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

Abstract

Extracted data

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

Abstract

Extracted data

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