Measurements of the surface flows, heat transfer, pressure distribution, and longitudinal stability of a mercury capsule model at Mach numbers of 6.9 and 9.6 /

Experimental pressure distributions on a blunt lifting-entry body at Mach 3.71 /

Morris, W. Douglas.
Couch, Lana M.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."April 1968."Includes bibliographical references (p. 12).Mode of access: Internet

Flight test aerodynamic heating data for the afterbody of the Project Mercury spacecraft with comparisons to available prediction methods /

Murphy, J. D.
Project Mercury (U.S.)
Manned Spacecraft Center (U.S.)
Lockheed Missiles and Space Company.
United States. National Aeronautics and Space Administration.

January 1967

"June 1967."Includes bibliographical references."Prepared under contract no.Mode of access: Internet

Laminar heat-transfer and pressure-distribution studies on a series of reentry nose shapes at a mach number of 19.4 in helium. /

Wagner, Richard D.
Henderson, Arthur, 1922-
Pine, W. Clint.
United States. National Aeronautics and Space Administration.

Cover title."June 1961."Aerodynamics, missiles and space vehicles; Fluid mechanics.Includes bibliogr...

Pressure and heat-transfer measurements on a Mercury capsule model /

Reller, John O.
Seegmiller, H. Lee.
Ames Research Center.

January 1962

"May 1962."Cover title.Includes bibliographical references (p. 38-41).Mode of access: Internet

Heat-transfer and pressure measurements of a 1/7-scale model of a Mercury capsule at angles of attack from 0° to ±20° at mach numbers of 3.50 and 4.44 /

Taylor, Nancy L.
Burbank, Paige B.
Hodge, Ward F.
United States. National Aeronautics and Space Administration.

January 1961

Mercury capsule heat shield - heat transfer and pressure coefficients at supersonic speeds."June 196...

Pressure and heat-transfer distribution on the afterbody of a lifting Mercury-type capsule at Mach number 15 in helium /

Marvin, Joseph G.
Ames Research Center.

January 1963

"April 1963."Cover title.Includes bibliographical references (p. 13-14).Mode of access: Internet

A compilation of wind-tunnel heat-transfer measurements on the afterbody of the Project Mercury capsule reentry configuration /

Weston, Kenneth C.
Swanson, Joanna E.
United States. National Aeronautics and Space Administration. Space Task Group.

January 1961

"August 1961."Cover title.Includes bibliographical references (p. 13-14).Mode of access: Internet

Wind-tunnel investigation at mach numbers from 0.50 to 1.14 of the static aerodynamic characteristics of a model of a Project Mercury capsule /

Pearson, Albin O.
United States. National Aeronautics and Space Administration.

"July 1960."Cover title.Includes bibliographical references (p. 6).Mode of access: Internet

Wind-tunnel investigation of static aerodynamic characteristics of a 1/9-scale model of a Project Mercury capsule at mach numbers from 1.60 to 4.65 /

Shaw, David S.
Turner, Kenneth L.
United States. National Aeronautics and Space Administration.

"July 1960."Cover title.Includes bibliographical references (p. 7).Mode of access: Internet

Heat-transfer and pressure measurements on a concove-nose cylinder for a mach number range of 2.49 to 4.44 /

Stallings, Jr., Robert L.
Burbank, Paige B.
Langley Research Center.

January 1959

"October 1959"--Cover.Caption title.Includes bibliographical references (p. 10).Mode of access: Inte...

Dynamic model tests at low subsonic speeds of Project Mercury capsule configurations with and without drogue parachutes /

Bowman, James S.
United States. National Aeronautics and Space Administration.

January 1961

"February 1961."Includes bibliographical references (p. 9).Mode of access: Internet

Heat-transfer measurements on a blunt spherical-segment nose to a Mach number of 15.1 and flight performance of the rocket-propelled model to a Mach number of 17.8 /

Rumsey, Charles B.
Lee, Dorothy B.
Langley Research Center.

January 1959

"November 1959."Cover title.Includes bibliographical references (p. 17-18).Mode of access: Internet

Effects of canted forward faces on the static longitudinal stability characteristics of the escape and exit configurations of a project mercury capsule model at a mach number of 2.01 /

Harris, Roy V.
Robinson, Ross B.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1960

"October 1960."Cover title.Includes bibliographical references (p. 5).Mode of access: Internet

Measurements of flow properties in the vicinity of three wing-fuselage combinations at Mach numbers of 1.61 and 2.01 /

Carlson, Harry W.
Langley Research Center.

January 1959

"October 1959."Cover title.Includes bibliographical references (p. 15).Mode of access: Internet

Pressure measurements on a hypersonic glide configuration having 79.5° sweepback and 45° dihedral at a Mach number of 4.95 /

Cooper, Morton.
Gunn, Charles R.
Langley Research Center.

January 1959

"November 1959"--Cover.Caption title.Includes bibliographical references (p. 8).Mode of access: Inte...

Experimental pressure distributions on a blunt lifting-entry body at Mach 3.71 /

Morris, W. Douglas.
Couch, Lana M.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."April 1968."Includes bibliographical references (p. 12).Mode of access: Internet

Flight test aerodynamic heating data for the afterbody of the Project Mercury spacecraft with comparisons to available prediction methods /

Murphy, J. D.
Project Mercury (U.S.)
Manned Spacecraft Center (U.S.)
Lockheed Missiles and Space Company.
United States. National Aeronautics and Space Administration.

January 1967

"June 1967."Includes bibliographical references."Prepared under contract no.Mode of access: Internet

Laminar heat-transfer and pressure-distribution studies on a series of reentry nose shapes at a mach number of 19.4 in helium. /

Wagner, Richard D.
Henderson, Arthur, 1922-
Pine, W. Clint.
United States. National Aeronautics and Space Administration.

Cover title."June 1961."Aerodynamics, missiles and space vehicles; Fluid mechanics.Includes bibliogr...

Pressure and heat-transfer measurements on a Mercury capsule model /

Reller, John O.
Seegmiller, H. Lee.
Ames Research Center.

January 1962

"May 1962."Cover title.Includes bibliographical references (p. 38-41).Mode of access: Internet

Heat-transfer and pressure measurements of a 1/7-scale model of a Mercury capsule at angles of attack from 0° to ±20° at mach numbers of 3.50 and 4.44 /

Taylor, Nancy L.
Burbank, Paige B.
Hodge, Ward F.
United States. National Aeronautics and Space Administration.

January 1961

Mercury capsule heat shield - heat transfer and pressure coefficients at supersonic speeds."June 196...

Pressure and heat-transfer distribution on the afterbody of a lifting Mercury-type capsule at Mach number 15 in helium /

Marvin, Joseph G.
Ames Research Center.

January 1963

"April 1963."Cover title.Includes bibliographical references (p. 13-14).Mode of access: Internet

A compilation of wind-tunnel heat-transfer measurements on the afterbody of the Project Mercury capsule reentry configuration /

Weston, Kenneth C.
Swanson, Joanna E.
United States. National Aeronautics and Space Administration. Space Task Group.

January 1961

"August 1961."Cover title.Includes bibliographical references (p. 13-14).Mode of access: Internet

Wind-tunnel investigation at mach numbers from 0.50 to 1.14 of the static aerodynamic characteristics of a model of a Project Mercury capsule /

Pearson, Albin O.
United States. National Aeronautics and Space Administration.

"July 1960."Cover title.Includes bibliographical references (p. 6).Mode of access: Internet

Wind-tunnel investigation of static aerodynamic characteristics of a 1/9-scale model of a Project Mercury capsule at mach numbers from 1.60 to 4.65 /

Shaw, David S.
Turner, Kenneth L.
United States. National Aeronautics and Space Administration.

"July 1960."Cover title.Includes bibliographical references (p. 7).Mode of access: Internet

Heat-transfer and pressure measurements on a concove-nose cylinder for a mach number range of 2.49 to 4.44 /

Stallings, Jr., Robert L.
Burbank, Paige B.
Langley Research Center.

January 1959

"October 1959"--Cover.Caption title.Includes bibliographical references (p. 10).Mode of access: Inte...

Dynamic model tests at low subsonic speeds of Project Mercury capsule configurations with and without drogue parachutes /

Bowman, James S.
United States. National Aeronautics and Space Administration.

January 1961

"February 1961."Includes bibliographical references (p. 9).Mode of access: Internet

Heat-transfer measurements on a blunt spherical-segment nose to a Mach number of 15.1 and flight performance of the rocket-propelled model to a Mach number of 17.8 /

Rumsey, Charles B.
Lee, Dorothy B.
Langley Research Center.

January 1959

"November 1959."Cover title.Includes bibliographical references (p. 17-18).Mode of access: Internet

Effects of canted forward faces on the static longitudinal stability characteristics of the escape and exit configurations of a project mercury capsule model at a mach number of 2.01 /

Harris, Roy V.
Robinson, Ross B.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1960

"October 1960."Cover title.Includes bibliographical references (p. 5).Mode of access: Internet

Measurements of flow properties in the vicinity of three wing-fuselage combinations at Mach numbers of 1.61 and 2.01 /

Carlson, Harry W.
Langley Research Center.

January 1959

"October 1959."Cover title.Includes bibliographical references (p. 15).Mode of access: Internet

Pressure measurements on a hypersonic glide configuration having 79.5° sweepback and 45° dihedral at a Mach number of 4.95 /

Cooper, Morton.
Gunn, Charles R.
Langley Research Center.

January 1959

"November 1959"--Cover.Caption title.Includes bibliographical references (p. 8).Mode of access: Inte...

Experimental pressure distributions on a blunt lifting-entry body at Mach 3.71 /

Morris, W. Douglas.
Couch, Lana M.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."April 1968."Includes bibliographical references (p. 12).Mode of access: Internet

Flight test aerodynamic heating data for the afterbody of the Project Mercury spacecraft with comparisons to available prediction methods /

Murphy, J. D.
Project Mercury (U.S.)
Manned Spacecraft Center (U.S.)
Lockheed Missiles and Space Company.
United States. National Aeronautics and Space Administration.

January 1967

"June 1967."Includes bibliographical references."Prepared under contract no.Mode of access: Internet

Laminar heat-transfer and pressure-distribution studies on a series of reentry nose shapes at a mach number of 19.4 in helium. /

Wagner, Richard D.
Henderson, Arthur, 1922-
Pine, W. Clint.
United States. National Aeronautics and Space Administration.

Cover title."June 1961."Aerodynamics, missiles and space vehicles; Fluid mechanics.Includes bibliogr...

Measurements of the surface flows, heat transfer, pressure distribution, and longitudinal stability of a mercury capsule model at Mach numbers of 6.9 and 9.6 /

Abstract

Extracted data

Measurements of the surface flows, heat transfer, pressure distribution, and longitudinal stability of a mercury capsule model at Mach numbers of 6.9 and 9.6 /

Abstract

Extracted data

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