Ojas Tyagi Email and Phone Number

Non-metallics testing,Rubber components,Safety standards, Mechanical testing, Tool design.

• Perform complex electro-mechanical technical functions and activities such as design, test, checkout, fabrication, modification, troubleshooting and assembly of electronics and electro-mechanical systems • Experimental design circuitry, prototype models, specialized test equipment, tools, and test fixtures.• Perform new system and NPI installations and field upgrades, practice 6S, utilize LEAN tools.• Troubleshoot of system level and component level problems in electrical and mechanical systems and sub-systems. DMA analysis, Material Characterization processDevelop and implement quality control procedures and inspection plans to ensure adherence to industry standards and customer specifications.• Conduct regular audits of production processes, identifying potential non-conformances and recommending corrective actions.• Collaborate with cross-functional teams to address quality-related issues and drive continuous improvement projects.• Perform root cause analysis and utilize statistical methods to analyze data and identify trends for process improvement.• Led a team to successfully reduce defect rate through the implementation of Six Sigma. HASS and DFR Principles.• Coordinate with suppliers to resolve quality issues and improve incoming materials' quality ISO 14001.

Quality & Reliability: Study of Fatigue Life Prediction of solder joint of Opto-electronics package Reliability of 2.5D electronic package.Optimized its design using Ansys Mechanical (FEA) and calculated its Fatigue Life to failure, improved product life cycle and improvementprocess and maintained ISO Aerospace Quality Standards. HALT under JEDEC.Designed, executed, and oversaw reliability and serviceability tests such as accelerated life testing, environmental stress screening, HALT, and HASS.

Basic PYTHON programming using DJANGO framework and designed desktop based application

Conducted Design and analysis of solar UAV that included Aircraft design and CFD analysis using ANSYS and CATIA. The UAV achieved 24 hr endurance.

Was given a task in basic CFD analysis of airfoil and structural design using PATRAN software for UAV