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

Comparison of experimental and theoretical shock shapes and pressure distributions on flat-faced cylinders at Mach 10.5 /

Inouye, Mamoru.
Sinclair, A. Richard.
Marvin, Joseph G.
Ames Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."February 1968."Includes bibliographical references (p. 8).Mode of access: Internet

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

Denardo, B. Pat.
United States. National Aeronautics and Space Administration.

Cover title."March 1962."Materials, engineering; Structures.Includes bibliographical references.Mode...

Predicted shock envelopes about two types of vehicles at large angles of attack /

Kaattari, George E.
United States. National Aeronautics and Space Administration.

Cover title."April 1961."Aerodynamics, missiles and space vehicles; Fluid mechanics.Includes bibliog...

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

Hypervelocity impact physics /

Schonberg, William P.
Darzi, Kent.
Bean, Alan J.
George C. Marshall Space Flight Center.
University of Alabama in Huntsville. Dept. of Mechanical Engineering.

January 1991

Prepared at the University of Alabama in Huntsville, Dept. of Mechanical Engineering, for George C. ...

Hypervelocity impacts into stainless-steel tubes armored with reinforced beryllium /

McMillan, A. R.
Diedrich, James H.
Clough, Nestor.
United States. National Aeronautics and Space Administration.

"Jul 1966" -- Cover."N6631354."Includes bibliographical references (p. 15-16).Mode of access: Intern...

Hypervelocity micro-particle impact on thin foils /

Richards L. G.
Gehring, J. W. Jr.
U.S. Army Ballistic Research Laboratory.

"Department of the Army Project No. 503-04-11; Ordnance Management Structure Code No. 5010.11.833.""...

Hypersonic research in the shock tunnel.

Wittliff, Charles E.

"Presented at the I.A.S. National Symposium on Hypervelocity Techniques, Denver, Colorado, October 2...

Hypervelocity impact testing of cables /

Jex, David W.
George C. Marshall Space Flight Center.

January 1973

Prepared at George C. Marshall Space Flight Center.Cover title.Bibliography: p. 53.Mode of access: I...

Theory of an electromagnetic mass accelerator for achieving hypervelocities. /

Thom, Karlheinz.
United States. National Aeronautics and Space Administration.

Cover title."June 1961."Fluid mechanics; Research and development facilities.Includes bibliographica...

Crater characteristics of 11 metal alloys under hyper-velocity impact including effects of projectile density and target temperature /

Clough, Nestor.
McMillan, A. R.
Lieblein, Seymour.
United States. National Aeronautics and Space Administration.
Lewis Research Center.

Prepared at Lewis Research Center."April 1969"--Cover.Includes bibliographical references (p. 25-26)...

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...

A method for determining surface pressures on blunt bodies of revolution at small angles of attack in supersonic flow /

Jackson, Charlie M.
Smith, Rudeen S.
Sawyer, Wallace C.
United States. National Aeronautics and Space Administration.

Cover title."November 1968."Includes bibliographical references.Mode of access: Internet

Correlation of new hypervelocity impact data by threshold penetration relations

Hayduk, Robert J.
Alfaro-Bou, Emilio.
Gough, Paul S.
United States. National Aeronautics and Space Administration.
Langley Research Center.

January 1973

Threshold penetration data are established by impacting spherical projectiles onto 2024 aluminum sin...

Study of hypervelocity micro-particle cratering /

Richards L. G.
Holloway, L. S.
U.S. Atomic Energy Commission.
U.S. Army Ballistic Research Laboratory.

"Department of the Army Project No. 5B03-04-011; Ordnance Management Structure Code No. 5010.11.833;...

Comparison of experimental and theoretical shock shapes and pressure distributions on flat-faced cylinders at Mach 10.5 /

Inouye, Mamoru.
Sinclair, A. Richard.
Marvin, Joseph G.
Ames Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."February 1968."Includes bibliographical references (p. 8).Mode of access: Internet

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

Denardo, B. Pat.
United States. National Aeronautics and Space Administration.

Cover title."March 1962."Materials, engineering; Structures.Includes bibliographical references.Mode...

Predicted shock envelopes about two types of vehicles at large angles of attack /

Kaattari, George E.
United States. National Aeronautics and Space Administration.

Cover title."April 1961."Aerodynamics, missiles and space vehicles; Fluid mechanics.Includes bibliog...

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

Hypervelocity impact physics /

Schonberg, William P.
Darzi, Kent.
Bean, Alan J.
George C. Marshall Space Flight Center.
University of Alabama in Huntsville. Dept. of Mechanical Engineering.

January 1991

Prepared at the University of Alabama in Huntsville, Dept. of Mechanical Engineering, for George C. ...

Hypervelocity impacts into stainless-steel tubes armored with reinforced beryllium /

McMillan, A. R.
Diedrich, James H.
Clough, Nestor.
United States. National Aeronautics and Space Administration.

"Jul 1966" -- Cover."N6631354."Includes bibliographical references (p. 15-16).Mode of access: Intern...

Hypervelocity micro-particle impact on thin foils /

Richards L. G.
Gehring, J. W. Jr.
U.S. Army Ballistic Research Laboratory.

"Department of the Army Project No. 503-04-11; Ordnance Management Structure Code No. 5010.11.833.""...

Hypersonic research in the shock tunnel.

Wittliff, Charles E.

"Presented at the I.A.S. National Symposium on Hypervelocity Techniques, Denver, Colorado, October 2...

Hypervelocity impact testing of cables /

Jex, David W.
George C. Marshall Space Flight Center.

January 1973

Prepared at George C. Marshall Space Flight Center.Cover title.Bibliography: p. 53.Mode of access: I...

Theory of an electromagnetic mass accelerator for achieving hypervelocities. /

Thom, Karlheinz.
United States. National Aeronautics and Space Administration.

Cover title."June 1961."Fluid mechanics; Research and development facilities.Includes bibliographica...

Crater characteristics of 11 metal alloys under hyper-velocity impact including effects of projectile density and target temperature /

Clough, Nestor.
McMillan, A. R.
Lieblein, Seymour.
United States. National Aeronautics and Space Administration.
Lewis Research Center.

Prepared at Lewis Research Center."April 1969"--Cover.Includes bibliographical references (p. 25-26)...

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...

A method for determining surface pressures on blunt bodies of revolution at small angles of attack in supersonic flow /

Jackson, Charlie M.
Smith, Rudeen S.
Sawyer, Wallace C.
United States. National Aeronautics and Space Administration.

Cover title."November 1968."Includes bibliographical references.Mode of access: Internet

Correlation of new hypervelocity impact data by threshold penetration relations

Hayduk, Robert J.
Alfaro-Bou, Emilio.
Gough, Paul S.
United States. National Aeronautics and Space Administration.
Langley Research Center.

January 1973

Threshold penetration data are established by impacting spherical projectiles onto 2024 aluminum sin...

Study of hypervelocity micro-particle cratering /

Richards L. G.
Holloway, L. S.
U.S. Atomic Energy Commission.
U.S. Army Ballistic Research Laboratory.

"Department of the Army Project No. 5B03-04-011; Ordnance Management Structure Code No. 5010.11.833;...

Comparison of experimental and theoretical shock shapes and pressure distributions on flat-faced cylinders at Mach 10.5 /

Inouye, Mamoru.
Sinclair, A. Richard.
Marvin, Joseph G.
Ames Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."February 1968."Includes bibliographical references (p. 8).Mode of access: Internet

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

Denardo, B. Pat.
United States. National Aeronautics and Space Administration.

Cover title."March 1962."Materials, engineering; Structures.Includes bibliographical references.Mode...

Predicted shock envelopes about two types of vehicles at large angles of attack /

Kaattari, George E.
United States. National Aeronautics and Space Administration.

Cover title."April 1961."Aerodynamics, missiles and space vehicles; Fluid mechanics.Includes bibliog...

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

Abstract

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

Abstract

Extracted data

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