Viking entry vehicle aerodynamics at M = 2 in air and some preliminary test data for flight in CO₂ at M = 11 /

Aerodynamic characteristics of a 1/6-scale model of the rotor systems research aircraft with the rotors removed /

Mineck, Raymond E.
Hassell, James L., joint author.
Freeman, Carl E., joint author.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1976

Cover title.Includes bibliographical references (p. 23).Mode of access: Internet

Hypersonic aerodynamics and entry-maneuver--aerothermodynamic interactions for two lifting entry vehicles /

Arrington, James P.
Woods, William C.
Langley Research Center.

January 1972

Prepared at Langley Research Center.Cover title.Bibliography: p. 12.Mode of access: Internet

Investigation of the aerodynamic characteristics of two preliminary designs of Scout research vehicle at Mach numbers from 1.77 to 4.65 /

Keynton, Robert J.
Fichter, Ann B.
Langley Research Center.

Prepared at Langley Research Center."April 1961."Cover title.Includes bibliographical references (p....

Flight tests of Viking parachute system in three Mach number regimes /

Lundstrom, Reginald R.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references.1. Vehicle descr...

Postflight simulation of parachute deployment dynamics of Viking qualification flight tests /

Whitlock, Charles H.
Talay, Theodore A.
Poole, Lamont R. (Lamont Rozelle)
Langley Research Center.

January 1973

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 14-15).Mode ...

Experimental investigation at Mach 8 of the effects of projections and cavities on heat transfer to a model of the Viking aeroshell /

Creel, Theodore R.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 7).Mode of a...

Aerodynamic testing technique for twin-fuselage models at hypersonic speeds /

Ashby, George C.
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 6).Mode of a...

Determination of the hypersonic-continuum/rarefield-flow drag coefficient of the Viking Lander Capsule 1 aeroshell from flight data /

Blanchard, Robert C.
Walberg, Gerald D.
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

Flight-test investigation of the aerodynamic characteristics and flow interference effects about the aft fuselage of the F111A airplane /

Taillon, Norman V.
Flight Research Center (U.S.)

January 1974

Prepared at the NASA Flight Research Center.Cover title.Includes bibliographical references (p. 14)....

Experimental aerodynamic performance characteristics of a rotor entry vehicle configuration : II. Transonic /

Levin, Alan D.
Smith, Ronald C. (Ronald Carlton)
United States. National Aeronautics and Space Administration.
Ames Research Center.

January 1971

Prepared at Ames Research Center.N71-16534.February 1971.Includes bibliographical references (p. 9)....

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 ...

Exploratory investigation of the aerodynamic characteristics of a biwing vehicle at Mach 20.3 /

Bernot, Peter T.
Langley Research Center.

January 1985

Prepared at Langley Research Center."February 1985"--Cover.Includes bibliographical references (p. 4...

Aerodynamic and landing measurements obtained during the first powered flight of the North American X-15 research airplane /

United States. National Aeronautics and Space Administration.
Flight Research Center (U.S.)

"January 1960."Cover title.Includes bibliographical references (p. 17).Mode of access: Internet

Experimental aerodynamic performance characteristics of a rotor entry vehicle configuration : I. Subsonic /

Smith, Ronald C. (Ronald Carlton)
Levin, Alan D.
United States. National Aeronautics and Space Administration.
Ames Research Center.

January 1971

Prepared at Ames Research Center.N71-16533.February 1971.Includes bibliographical references (p. 10)...

Experimental aerodynamic performance characteristics of a rotor entry vehicle configuration : III. Supersonic /

Smith, Ronald C. (Ronald Carlton)
Levin, Alan D.
United States. National Aeronautics and Space Administration.
Ames Research Center.

January 1971

Prepared at Ames Research Center.N71-16535.February 1971.Includes bibliographical references (p. 10)...

Aerodynamic characteristics of a 1/6-scale model of the rotor systems research aircraft with the rotors removed /

Mineck, Raymond E.
Hassell, James L., joint author.
Freeman, Carl E., joint author.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1976

Cover title.Includes bibliographical references (p. 23).Mode of access: Internet

Hypersonic aerodynamics and entry-maneuver--aerothermodynamic interactions for two lifting entry vehicles /

Arrington, James P.
Woods, William C.
Langley Research Center.

January 1972

Prepared at Langley Research Center.Cover title.Bibliography: p. 12.Mode of access: Internet

Investigation of the aerodynamic characteristics of two preliminary designs of Scout research vehicle at Mach numbers from 1.77 to 4.65 /

Keynton, Robert J.
Fichter, Ann B.
Langley Research Center.

Prepared at Langley Research Center."April 1961."Cover title.Includes bibliographical references (p....

Flight tests of Viking parachute system in three Mach number regimes /

Lundstrom, Reginald R.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references.1. Vehicle descr...

Postflight simulation of parachute deployment dynamics of Viking qualification flight tests /

Whitlock, Charles H.
Talay, Theodore A.
Poole, Lamont R. (Lamont Rozelle)
Langley Research Center.

January 1973

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 14-15).Mode ...

Experimental investigation at Mach 8 of the effects of projections and cavities on heat transfer to a model of the Viking aeroshell /

Creel, Theodore R.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 7).Mode of a...

Aerodynamic testing technique for twin-fuselage models at hypersonic speeds /

Ashby, George C.
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 6).Mode of a...

Determination of the hypersonic-continuum/rarefield-flow drag coefficient of the Viking Lander Capsule 1 aeroshell from flight data /

Blanchard, Robert C.
Walberg, Gerald D.
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

Flight-test investigation of the aerodynamic characteristics and flow interference effects about the aft fuselage of the F111A airplane /

Taillon, Norman V.
Flight Research Center (U.S.)

January 1974

Prepared at the NASA Flight Research Center.Cover title.Includes bibliographical references (p. 14)....

Experimental aerodynamic performance characteristics of a rotor entry vehicle configuration : II. Transonic /

Levin, Alan D.
Smith, Ronald C. (Ronald Carlton)
United States. National Aeronautics and Space Administration.
Ames Research Center.

January 1971

Prepared at Ames Research Center.N71-16534.February 1971.Includes bibliographical references (p. 9)....

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 ...

Exploratory investigation of the aerodynamic characteristics of a biwing vehicle at Mach 20.3 /

Bernot, Peter T.
Langley Research Center.

January 1985

Prepared at Langley Research Center."February 1985"--Cover.Includes bibliographical references (p. 4...

Aerodynamic and landing measurements obtained during the first powered flight of the North American X-15 research airplane /

United States. National Aeronautics and Space Administration.
Flight Research Center (U.S.)

"January 1960."Cover title.Includes bibliographical references (p. 17).Mode of access: Internet

Experimental aerodynamic performance characteristics of a rotor entry vehicle configuration : I. Subsonic /

Smith, Ronald C. (Ronald Carlton)
Levin, Alan D.
United States. National Aeronautics and Space Administration.
Ames Research Center.

January 1971

Prepared at Ames Research Center.N71-16533.February 1971.Includes bibliographical references (p. 10)...

Experimental aerodynamic performance characteristics of a rotor entry vehicle configuration : III. Supersonic /

Smith, Ronald C. (Ronald Carlton)
Levin, Alan D.
United States. National Aeronautics and Space Administration.
Ames Research Center.

January 1971

Prepared at Ames Research Center.N71-16535.February 1971.Includes bibliographical references (p. 10)...

Aerodynamic characteristics of a 1/6-scale model of the rotor systems research aircraft with the rotors removed /

Mineck, Raymond E.
Hassell, James L., joint author.
Freeman, Carl E., joint author.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1976

Cover title.Includes bibliographical references (p. 23).Mode of access: Internet

Hypersonic aerodynamics and entry-maneuver--aerothermodynamic interactions for two lifting entry vehicles /

Arrington, James P.
Woods, William C.
Langley Research Center.

January 1972

Prepared at Langley Research Center.Cover title.Bibliography: p. 12.Mode of access: Internet

Investigation of the aerodynamic characteristics of two preliminary designs of Scout research vehicle at Mach numbers from 1.77 to 4.65 /

Keynton, Robert J.
Fichter, Ann B.
Langley Research Center.

Prepared at Langley Research Center."April 1961."Cover title.Includes bibliographical references (p....

Viking entry vehicle aerodynamics at M = 2 in air and some preliminary test data for flight in CO₂ at M = 11 /

Abstract

Extracted data

Viking entry vehicle aerodynamics at M = 2 in air and some preliminary test data for flight in CO₂ at M = 11 /

Abstract

Extracted data

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