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

Supersonic Aerodynamic Characteristics and Shock Standoff Distances for Large-Angle Cones with and Without Cylindrical Afterbodies

Campbell, James F.

August 1969

Supersonic aerodynamic characteristics and shock standoff distances for large angle cones with and w...

Performance of a 16.6-meter-diameter cross parachute in a simulated Martian environment

Lundstrom, R. R.
Darnell, W. L.
Coltrane, L. C.

April 1968

Inflation and drag characteristics of cross parachute in simulated Martian environmen

Experimental wake survey behind a 120 deg included angle cone at angles of attack of 0 deg and 5 deg, Mach numbers from 1.60 to 3.95, and longitudinal stations varying from 1.0 to 8.39 body diameters

Brown, C. A., Jr.
Tudor, D. H.
Campbell, J. F.

January 1971

Wake flow properties of conical bodies at supersonic speeds and various angles of attac

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...

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

Intrieri, P. F.

May 1965

Static and dynamic stability, and drag characteristics of conical nosed planetary vehicle during atm...

Low subsonic static and dynamic stability characteristics of two blunt 120 deg cone configurations

Bendura, R. J.

February 1967

Low subsonic static and dynamic stability characteristics of blunt 120 deg conical configuratio

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...

Flight test of a 15-foot-diameter /4.6-meter/ 120 deg conical spacecraft simulating parachute deployment in a Mars atmosphere

Darnell, W. L.
Lundstrom, R. R.
Henning, A. B.

December 1967

Flight test of conical spacecraft simulating parachute deployment in Mars atmospher

Low subsonic dynamic-stability investigation of several planetary-entry configurations in a vertical wind tunnel, part i

Marte, J. E.
Weaver, R. W.

April 1965

Low subsonic dynamic stability data for evaluation of ballistic deceleration vehicle entering Mars a...

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-...

Flight test of an erectable spacecraft used for decelerator testing at simulated Mars entry conditions

Henning, A. B.
Lundstrom, R. R.

October 1972

A 55 foot diameter disk-gap-band parachute was deployed behind an expandable 15 foot diameter, 120 d...

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

Stability Investigation of a Blunted Cone and a Blunted Ogive with a Flared Cylinder Afterbody at Mach Numbers from 0.30 to 2.85

Coltrane, Lucille C.

November 1959

A cone with a blunt nose tip and a 10.7 deg cone half angle and an ogive with a blunt nose tip and a...

Dynamic-model study of planetary-entry configurations in the Langley spin tunnel

Costigan, P. J.

July 1966

Dynamic model study to determine low subsonic speed stability and drag characteristics during vertic...

Aerodynamic characteristics of a modified cone - Conical-frustum entry configuration at Mach 6.0

Ashby, G. C., Jr.
Staylor, W. F.

June 1968

Aerodynamic characteristics of modified conical lifting reentry vehicle at hypersonic speed

Supersonic Aerodynamic Characteristics and Shock Standoff Distances for Large-Angle Cones with and Without Cylindrical Afterbodies

Campbell, James F.

August 1969

Supersonic aerodynamic characteristics and shock standoff distances for large angle cones with and w...

Performance of a 16.6-meter-diameter cross parachute in a simulated Martian environment

Lundstrom, R. R.
Darnell, W. L.
Coltrane, L. C.

April 1968

Inflation and drag characteristics of cross parachute in simulated Martian environmen

Experimental wake survey behind a 120 deg included angle cone at angles of attack of 0 deg and 5 deg, Mach numbers from 1.60 to 3.95, and longitudinal stations varying from 1.0 to 8.39 body diameters

Brown, C. A., Jr.
Tudor, D. H.
Campbell, J. F.

January 1971

Wake flow properties of conical bodies at supersonic speeds and various angles of attac

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...

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

Intrieri, P. F.

May 1965

Static and dynamic stability, and drag characteristics of conical nosed planetary vehicle during atm...

Low subsonic static and dynamic stability characteristics of two blunt 120 deg cone configurations

Bendura, R. J.

February 1967

Low subsonic static and dynamic stability characteristics of blunt 120 deg conical configuratio

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...

Flight test of a 15-foot-diameter /4.6-meter/ 120 deg conical spacecraft simulating parachute deployment in a Mars atmosphere

Darnell, W. L.
Lundstrom, R. R.
Henning, A. B.

December 1967

Flight test of conical spacecraft simulating parachute deployment in Mars atmospher

Low subsonic dynamic-stability investigation of several planetary-entry configurations in a vertical wind tunnel, part i

Marte, J. E.
Weaver, R. W.

April 1965

Low subsonic dynamic stability data for evaluation of ballistic deceleration vehicle entering Mars a...

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-...

Flight test of an erectable spacecraft used for decelerator testing at simulated Mars entry conditions

Henning, A. B.
Lundstrom, R. R.

October 1972

A 55 foot diameter disk-gap-band parachute was deployed behind an expandable 15 foot diameter, 120 d...

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

Stability Investigation of a Blunted Cone and a Blunted Ogive with a Flared Cylinder Afterbody at Mach Numbers from 0.30 to 2.85

Coltrane, Lucille C.

November 1959

A cone with a blunt nose tip and a 10.7 deg cone half angle and an ogive with a blunt nose tip and a...

Dynamic-model study of planetary-entry configurations in the Langley spin tunnel

Costigan, P. J.

July 1966

Dynamic model study to determine low subsonic speed stability and drag characteristics during vertic...

Aerodynamic characteristics of a modified cone - Conical-frustum entry configuration at Mach 6.0

Ashby, G. C., Jr.
Staylor, W. F.

June 1968

Aerodynamic characteristics of modified conical lifting reentry vehicle at hypersonic speed

Supersonic Aerodynamic Characteristics and Shock Standoff Distances for Large-Angle Cones with and Without Cylindrical Afterbodies

Campbell, James F.

August 1969

Supersonic aerodynamic characteristics and shock standoff distances for large angle cones with and w...

Performance of a 16.6-meter-diameter cross parachute in a simulated Martian environment

Lundstrom, R. R.
Darnell, W. L.
Coltrane, L. C.

April 1968

Inflation and drag characteristics of cross parachute in simulated Martian environmen

Experimental wake survey behind a 120 deg included angle cone at angles of attack of 0 deg and 5 deg, Mach numbers from 1.60 to 3.95, and longitudinal stations varying from 1.0 to 8.39 body diameters

Brown, C. A., Jr.
Tudor, D. H.
Campbell, J. F.

January 1971

Wake flow properties of conical bodies at supersonic speeds and various angles of attac

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

Abstract

Extracted data

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

Abstract

Extracted data

Related items

Related items