Study of the stability and drag at mach numbers from 4.5 to 13.5 of a conical venus- entry body

Aerodynamic characteristics from mach 0.22 to 4.65 of a two-stage rocket vehicle having an unusual nose shape high power, high voltage, audio frequency transformer design manual final report, 1 jul. 1962 - 31 aug. 1964

Suttles, J. T.

November 1964

Transonic and supersonic aerodynamic characteristics for two-stage rocket vehicle with blunted nose ...

Measured pressure distributions, aerodynamic coefficients and shock shapes on blunt bodies at incidence in hypersonic air and CF4

Miller, C. G., III

September 1982

Pressure distributions, aerodynamic coefficients, and shock shapes were measured on blunt bodies of ...

Dynamics of high drag probe shapes at transonic speeds

Sammonds, R. I.

September 1971

Determination of transonic aerodynamic characteristics of spherically blunted 55 and 60 degree half-...

Experimental stability and drag of a pointed and a blunted 30 deg half-angle cone at Mach numbers from 11.5 to 34 in air

Intrieri, P. F.

January 1966

Static and dynamic stability and drag of blunted and pointed cones at various Mach numbers and Reyno...

Dynamic stability of a 4.6-meter-diameter 120 deg conical spacecraft at Mach numbers from 0.78 to 0.48 in a simulated Martian environment

Bendura, R. J.
Whitlock, C. H.

May 1968

Subsonic dynamic stability characteristics of large conical spacecraft in simulated Martian environm...

Aerodynamic heating of conical entry vehicles at speeds in excess of earth parabolic speed

Winovich, W.
Allen, H. J.
Seiff, A.

December 1963

Aerodynamic heating of conical vehicles entering earth atmosphere at speeds greater than earth parab...

Stability and drag characteristics at Mach numbers of 10 and 26 of a proposed slender atmospheric probe

Malcolm, G. N.

April 1967

Stability and drag characteristics of slender, flare-stabilized cone cylinder for Mars atmospheric p...

Aerodynamics of Mars entry probe-lander configurations at a Mach number of 10.

Sammonds, Robert I.
Ames Research Center.
United States. National Aeronautics and Space Administration.

Five spherically blunted cones were tested in free flight, in still air, to determine their aerodyna...

Real-gas effects on the drag and trajectories of a nonlifting 140 deg conical aeroshell during Mars entry

Bobbitt, P. J.
Allison, D. O.

February 1971

Real gas effects on drag and trajectories of nonlifting conical shell during Mars atmospheric entr

Static stability characteristics of several raked-off circular and elliptical cones at mach 6.7

Bernot, P. T.

October 1965

Static stability characteristics of circular and elliptical cones at hypersonic speed

Cone Angle Choices for Atmospheric Entry Vehicles: A Review

Tauber, Michael
Wright, Michael J.

June 2008

This presentation was part of the session : Historical PerspectivesSixth International Planetary Pro...

Studies in Support of Venus Aerocapture Utilizing Drag Modulation

Beck, Robin
Venkatapathy, Ethiraj
Aftosmis, Michael
Wercinski, Paul
Allen, Gary
Wilder, Mike

June 2018

Aerocapture has been extensively studied and these studies have shown the benefit for planetary expl...

Fluctuating pressures on the afterbodies of five blunt atmosphere entry vehicles

Robinson, R. C.
Gambucci, B. J.
George, R. E.

May 1968

Pressure fluctuation measurements on afterbodies of blunt atmospheric entry vehicle

Experimental investigation of hypersonic aerodynamics

Intrieri, Peter F.

July 1988

An extensive series of ballistic range tests were conducted at the Ames Research Center to determine...

Ballistic-range tests of a drag-ring configuration at Mach numbers around 2

De Rose, C. E.

December 1967

Unmanned Mars probe tested for drag, lift, static and dynamic stability at Mach number

Aerodynamic characteristics from mach 0.22 to 4.65 of a two-stage rocket vehicle having an unusual nose shape high power, high voltage, audio frequency transformer design manual final report, 1 jul. 1962 - 31 aug. 1964

Suttles, J. T.

November 1964

Transonic and supersonic aerodynamic characteristics for two-stage rocket vehicle with blunted nose ...

Measured pressure distributions, aerodynamic coefficients and shock shapes on blunt bodies at incidence in hypersonic air and CF4

Miller, C. G., III

September 1982

Pressure distributions, aerodynamic coefficients, and shock shapes were measured on blunt bodies of ...

Dynamics of high drag probe shapes at transonic speeds

Sammonds, R. I.

September 1971

Determination of transonic aerodynamic characteristics of spherically blunted 55 and 60 degree half-...

Experimental stability and drag of a pointed and a blunted 30 deg half-angle cone at Mach numbers from 11.5 to 34 in air

Intrieri, P. F.

January 1966

Static and dynamic stability and drag of blunted and pointed cones at various Mach numbers and Reyno...

Dynamic stability of a 4.6-meter-diameter 120 deg conical spacecraft at Mach numbers from 0.78 to 0.48 in a simulated Martian environment

Bendura, R. J.
Whitlock, C. H.

May 1968

Subsonic dynamic stability characteristics of large conical spacecraft in simulated Martian environm...

Aerodynamic heating of conical entry vehicles at speeds in excess of earth parabolic speed

Winovich, W.
Allen, H. J.
Seiff, A.

December 1963

Aerodynamic heating of conical vehicles entering earth atmosphere at speeds greater than earth parab...

Stability and drag characteristics at Mach numbers of 10 and 26 of a proposed slender atmospheric probe

Malcolm, G. N.

April 1967

Stability and drag characteristics of slender, flare-stabilized cone cylinder for Mars atmospheric p...

Aerodynamics of Mars entry probe-lander configurations at a Mach number of 10.

Sammonds, Robert I.
Ames Research Center.
United States. National Aeronautics and Space Administration.

Five spherically blunted cones were tested in free flight, in still air, to determine their aerodyna...

Real-gas effects on the drag and trajectories of a nonlifting 140 deg conical aeroshell during Mars entry

Bobbitt, P. J.
Allison, D. O.

February 1971

Real gas effects on drag and trajectories of nonlifting conical shell during Mars atmospheric entr

Static stability characteristics of several raked-off circular and elliptical cones at mach 6.7

Bernot, P. T.

October 1965

Static stability characteristics of circular and elliptical cones at hypersonic speed

Cone Angle Choices for Atmospheric Entry Vehicles: A Review

Tauber, Michael
Wright, Michael J.

June 2008

This presentation was part of the session : Historical PerspectivesSixth International Planetary Pro...

Studies in Support of Venus Aerocapture Utilizing Drag Modulation

Beck, Robin
Venkatapathy, Ethiraj
Aftosmis, Michael
Wercinski, Paul
Allen, Gary
Wilder, Mike

June 2018

Aerocapture has been extensively studied and these studies have shown the benefit for planetary expl...

Fluctuating pressures on the afterbodies of five blunt atmosphere entry vehicles

Robinson, R. C.
Gambucci, B. J.
George, R. E.

May 1968

Pressure fluctuation measurements on afterbodies of blunt atmospheric entry vehicle

Experimental investigation of hypersonic aerodynamics

Intrieri, Peter F.

July 1988

An extensive series of ballistic range tests were conducted at the Ames Research Center to determine...

Ballistic-range tests of a drag-ring configuration at Mach numbers around 2

De Rose, C. E.

December 1967

Unmanned Mars probe tested for drag, lift, static and dynamic stability at Mach number

Aerodynamic characteristics from mach 0.22 to 4.65 of a two-stage rocket vehicle having an unusual nose shape high power, high voltage, audio frequency transformer design manual final report, 1 jul. 1962 - 31 aug. 1964

Suttles, J. T.

November 1964

Transonic and supersonic aerodynamic characteristics for two-stage rocket vehicle with blunted nose ...

Measured pressure distributions, aerodynamic coefficients and shock shapes on blunt bodies at incidence in hypersonic air and CF4

Miller, C. G., III

September 1982

Pressure distributions, aerodynamic coefficients, and shock shapes were measured on blunt bodies of ...

Dynamics of high drag probe shapes at transonic speeds

Sammonds, R. I.

September 1971

Determination of transonic aerodynamic characteristics of spherically blunted 55 and 60 degree half-...

Study of the stability and drag at mach numbers from 4.5 to 13.5 of a conical venus- entry body

Abstract

Extracted data

Study of the stability and drag at mach numbers from 4.5 to 13.5 of a conical venus- entry body

Abstract

Extracted data

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