Aerojet Rocketdyne Jul 1988 - Jan 2014
Fellow, Materials Science and Engineering
Pratt & Whitney 1987 - 2012
Fellow-Structural Alloys
Education:
University of California, Los Angeles 1994 - 1997
Master of Science, Masters, Engineering
Columbia University In the City of New York 1983 - 1988
Bachelors, Bachelor of Science, Metallurgical Engineering
Skills:
Aerospace Engineering Engineering Management Materials Program Management Composites Continuous Improvement Earned Value Management Simulations Process Improvement Materials Science Mechanical Testing Material Selection Aerospace Engineering Process Engineering R&D Propulsion Alloys Failure Analysis Spacecraft Process Simulation Finite Element Analysis Stress Analysis Metallurgy Alloy Development Oxygen Compatibility Materials Processing
Monica Jacinto - Glendale CA, US Dallis Hardwick - Dayton OH, US
International Classification:
C22C019/05
US Classification:
420/446000, 148/428000
Abstract:
Burn-resistant metal alloys that also have a high tensile strength are described. The alloys generally include about 55 to about 75 weight percent nickel, about 12 to about 17 weight percent cobalt, about 4 to about 16 weight percent chromium, about 1 to about 4 weight percent aluminum, and about 1 to about 4 weight percent titanium.
Burn-Resistant And High Tensile Strength Metal Alloys
Monica Jacinto - Glendale CA, US Dallis Hardwick - Dayton OH, US
International Classification:
C22C019/05
US Classification:
420/446000
Abstract:
Burn-resistant metal alloys that also have a high tensile strength are described. The alloys generally include about 55 to about 75 weight percent nickel, about 12 to about 17 weight percent cobalt, about 4 to about 16 weight percent chromium, about 1 to about 4 weight percent aluminum, and about 1 to about 4 weight percent titanium.
Burn-Resistant And High Tensile Strength Metal Alloys
Monica A. Jacinto - Glendale CA, US Dallis Ann Hardwick - Dayton OH, US
International Classification:
C22C 19/05
US Classification:
420450, 420446
Abstract:
Burn-resistant metal alloys that also have a high tensile strength are described. The alloys generally include about 55 to about 75 weight percent nickel, about 12 to about 17 weight percent cobalt, about 4 to about 16 weight percent chromium, about 1 to about 4 weight percent aluminum, and about 1 to about 4 weight percent titanium.