Measurements of momentum transfer from plastic projectiles to massive aluminum targets at speeds up to 25,600 feet per second /

Pressure measurements on sharp and blunt 5 degreee and 15 degree-half-angle cones at mach number 3.86 and angles of attack to 100 degrees /

Amick, James L.
United States. National Aeronautics and Space Administration.

Cover title."February 1961."Aerodynamics, missiles and space vehicles; Fluid mechanics.Includes bibl...

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

The determination of ablative properties of materials in free-flight ranges /

Savin, Raymond C.
Dahms, Richard G.
Gloria, Hermilo R.
United States. National Aeronautics and Space Administration.

Cover title."June 1962."Aerodynamics, missiles and space vehicles; Atmospheric entry; Fluid mechanic...

An experimental investigation of the impact resistance of double-sheet structures at velocities to 24,000 feet per second /

Nysmith, C. Robert.
Summers, James L.
United States. National Aeronautics and Space Administration.

"October 1962."Cover title.Includes bibliographical references (p. 11).Mode of access: Internet

The dependency of penetration on the momentum per unit area of the impacting projectile and the resistance of materials to penetration /

Collins, Rufus Davis, 1932-
Kinard, William H.
Langley Research Center.

Prepared at Langley Research Center."May 1960."Cover title.Includes bibliographical references (p. 1...

The penetration of porous projectiles in aluminum and plastic targets /

Fish, Richard H.
Ames Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."April 1968."Includes bibliographical references (p. 5).Mode of access: Internet

Momentum accommodation of N⁺, N2⁺, and A⁺ incident on copper and aluminum from 0.5 to 4 kev /

Savage, Howard F. (Howard Frank)
Bader, Michel.
Ames Research Center.

Prepared at Ames Research Center."September 1963"--Cover.Includes bibliographical references (p. 9)....

Projectile size effects on hypervelocity impact craters in aluminum /

Denardo, B. Pat.
Nysmith, C. Robert.
Summers, James L.
Ames Research Center.
United States. National Aeronautics and Space Administration.

January 1967

Cover title."July 1967."Includes bibliographical references (p. 11).Mode of access: Internet

Experimental investigation of the momentum transfer associated with impact into thin aluminum targets

Nysmith, C.
Denardo, B.
Ames Research Center.
United States. National Aeronautics and Space Administration.

Momentum transfer from impact into thin aluminum meteor bumper targetsPrepared by Ames Research Cent...

A study of ballistic reentry trajectories at a velocity of 50,000 feet per second (15,240 meters per second) /

Suttles, John T.
Coltrane, Lucille C.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1967

Cover title."June 1967."Includes bibliographical references (p. 9).Mode of access: Internet

An investigation of spray velocity resulting from high-velocity penetration of thin plates by disks /

Di Battista, John D.
United States. National Aeronautics and Space Administration.

Cover title."September 1966."Includes bibliographical references.Mode of access: Internet

A preliminary investigation of the penetration of slender metal rods in thick metal targets /

Summers, James L., NASA researcher.
Niehaus, William R.
Ames Research Center.

January 1959

"NASA TN D-137.""Ames Research Center, Moffett Field, Calif.""December 1959."Title from cover.Includ...

Investigation of the lift, center of pressure, and drag of a projectile at Mach number of 8.6 and a Reynolds number of 17 million /

Canning, Thomas N.
Ames Research Center.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1954

"November 19, 1954."Includes bibliographical references (p. 12).Mode of access: Internet

A technique for obtaining hypervelocity impact data by using the relative hypervelocities of two projectiles /

Kinard, William H.
Collins, Rufus D.
United States. National Aeronautics and Space Administration.

Cover title." February 1961."Materials, engineering; Materials, other; Research and development faci...

The effect of vacuum on the penetration characteristics of projectiles into fine particles

Clark, Leonard V.
McCarty, John Locke.
United States. National Aeronautics and Space Administration.

Cover title."January 1963."Includes bibliographical references.Mode of access: Internet

Pressure measurements on sharp and blunt 5 degreee and 15 degree-half-angle cones at mach number 3.86 and angles of attack to 100 degrees /

Amick, James L.
United States. National Aeronautics and Space Administration.

Cover title."February 1961."Aerodynamics, missiles and space vehicles; Fluid mechanics.Includes bibl...

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

The determination of ablative properties of materials in free-flight ranges /

Savin, Raymond C.
Dahms, Richard G.
Gloria, Hermilo R.
United States. National Aeronautics and Space Administration.

Cover title."June 1962."Aerodynamics, missiles and space vehicles; Atmospheric entry; Fluid mechanic...

An experimental investigation of the impact resistance of double-sheet structures at velocities to 24,000 feet per second /

Nysmith, C. Robert.
Summers, James L.
United States. National Aeronautics and Space Administration.

"October 1962."Cover title.Includes bibliographical references (p. 11).Mode of access: Internet

The dependency of penetration on the momentum per unit area of the impacting projectile and the resistance of materials to penetration /

Collins, Rufus Davis, 1932-
Kinard, William H.
Langley Research Center.

Prepared at Langley Research Center."May 1960."Cover title.Includes bibliographical references (p. 1...

The penetration of porous projectiles in aluminum and plastic targets /

Fish, Richard H.
Ames Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."April 1968."Includes bibliographical references (p. 5).Mode of access: Internet

Momentum accommodation of N⁺, N2⁺, and A⁺ incident on copper and aluminum from 0.5 to 4 kev /

Savage, Howard F. (Howard Frank)
Bader, Michel.
Ames Research Center.

Prepared at Ames Research Center."September 1963"--Cover.Includes bibliographical references (p. 9)....

Projectile size effects on hypervelocity impact craters in aluminum /

Denardo, B. Pat.
Nysmith, C. Robert.
Summers, James L.
Ames Research Center.
United States. National Aeronautics and Space Administration.

January 1967

Cover title."July 1967."Includes bibliographical references (p. 11).Mode of access: Internet

Experimental investigation of the momentum transfer associated with impact into thin aluminum targets

Nysmith, C.
Denardo, B.
Ames Research Center.
United States. National Aeronautics and Space Administration.

Momentum transfer from impact into thin aluminum meteor bumper targetsPrepared by Ames Research Cent...

A study of ballistic reentry trajectories at a velocity of 50,000 feet per second (15,240 meters per second) /

Suttles, John T.
Coltrane, Lucille C.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1967

Cover title."June 1967."Includes bibliographical references (p. 9).Mode of access: Internet

An investigation of spray velocity resulting from high-velocity penetration of thin plates by disks /

Di Battista, John D.
United States. National Aeronautics and Space Administration.

Cover title."September 1966."Includes bibliographical references.Mode of access: Internet

A preliminary investigation of the penetration of slender metal rods in thick metal targets /

Summers, James L., NASA researcher.
Niehaus, William R.
Ames Research Center.

January 1959

"NASA TN D-137.""Ames Research Center, Moffett Field, Calif.""December 1959."Title from cover.Includ...

Investigation of the lift, center of pressure, and drag of a projectile at Mach number of 8.6 and a Reynolds number of 17 million /

Canning, Thomas N.
Ames Research Center.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1954

"November 19, 1954."Includes bibliographical references (p. 12).Mode of access: Internet

A technique for obtaining hypervelocity impact data by using the relative hypervelocities of two projectiles /

Kinard, William H.
Collins, Rufus D.
United States. National Aeronautics and Space Administration.

Cover title." February 1961."Materials, engineering; Materials, other; Research and development faci...

The effect of vacuum on the penetration characteristics of projectiles into fine particles

Clark, Leonard V.
McCarty, John Locke.
United States. National Aeronautics and Space Administration.

Cover title."January 1963."Includes bibliographical references.Mode of access: Internet

Pressure measurements on sharp and blunt 5 degreee and 15 degree-half-angle cones at mach number 3.86 and angles of attack to 100 degrees /

Amick, James L.
United States. National Aeronautics and Space Administration.

Cover title."February 1961."Aerodynamics, missiles and space vehicles; Fluid mechanics.Includes bibl...

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

The determination of ablative properties of materials in free-flight ranges /

Savin, Raymond C.
Dahms, Richard G.
Gloria, Hermilo R.
United States. National Aeronautics and Space Administration.

Cover title."June 1962."Aerodynamics, missiles and space vehicles; Atmospheric entry; Fluid mechanic...

Measurements of momentum transfer from plastic projectiles to massive aluminum targets at speeds up to 25,600 feet per second /

Abstract

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Measurements of momentum transfer from plastic projectiles to massive aluminum targets at speeds up to 25,600 feet per second /

Abstract

Extracted data

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