Working on the New Glenn Rocket systems Requirements for next generation landing system.

Most Recently driving schedule of the T55 Lube pump Safety of Flight Hardware for eventual first flight. Integration with other external systems and managing Production procurement specifications. Developing and executing Systems using DOORS for Verification and Validation for engine and control systems. Workstream Lead, Development Project Manager for Propulsion Controls, Turbo FansLeading Work teams on Wi-Fi enabled LRUs for advancing new product designs for the fleet.Managing integrated product teams, Control accounts, developing of milestones and project schedules.Recently changed process and removed barriers to be successful in the non travel remote work place. Trade Studies to drive new design concepts and SW/HW architecture of Engine ControllersLed SDLC (Software Development Life Cyle) for Universal Honeywell Propulsion Controller by leading (20) Software & System Engineer team across a matrixed organizationManaged Cost Account (CAM) for work stream, and framed IMS layouts for schedule fidelity.Successfully fulfilled requirements DOORs, including FAA, MIL, & FAR.Partnered across functional organization to develop quality and on time delivery with challenging schedule, for Customer First Flight Demo

Worked as a Principal Project Engineer on an Engine Controls System for propulsion engines.Developing requirements for implementation and integration with entire suite of engine LRUs (Line Replaceable Units)Worked in various disciplines of Business Aviation related to Turbo Fan Engines, Thrust Reversers and Nacelles. Project and Test Engineer, Repair and Over Haul, FAR 25 and 33, Design and Configuration Management.Additional Experience on Valves and Air Management systems for Dassault and Hawker Horizon Programs. Qualified pneumatic valve hardware to industry certification standards (RTCA DO160)Led a Lean Velocity Project team to increase efficiencies and replace old drawing release system.Supported Engine Test Programs for TFE 731-40, HTF7000 - AS907 Engines/ Nacelles and TF502/507.Worked with GKN suppliers to increase the quality of the Fan Cowl Door and nacelle hardware and maintain receipt deadlines.

Design Integration & Test Engineer, implementing engineering design changes and rework of hardware. Implemented in-house CNC methods to reduce costs and critical path.Vibration Test lab Scheduler/Manager of component hardware, 5S Leader, familiar with instrumentation and procurement.

Developed scheduling of resources and work around plans for critical path activities in order to support customer milestones and launch schedules.Managed multi-discipline (RF, Electrical, Propulsion, and Environmental) teams and planned resources to conduct testing and maintain standard flows of spacecraft in the Satellite Manufacturing Facility.Developed and maintained budgets and schedule goals related to CPI/SPI, wrote variances for out of scope activities. Proposal estimates for new integration work. Orion CAM used EVMS to monitor budgets and estimate team member support needs for Integration&Test. Responsible for variances for budgets and obtaining Management Reserves.Supported and successfully launched several satellites from various on-site locations. Cosmodrome in Kazakhstan, NASA Cape Canaveral and the ESA French Guiana space port. Responsible for meeting technical requirements of TAA contracts and deliverables of space craft and integrated payload of ITAR related hardware.Conducted various Test Readiness Reviews and Pre-ship Reviews for TVAC, Propulsion and EMI tests, and established cost accounts for I&T work.Reduced and maintained low levels of non-conformances and drove Root Cause Corrective Actions to completion, using TipQA.Managed teams to process, develop, release and execute Work Instructions and analysis to support I&T activities to build, process, and deliver Orion Flight hardware.Conducted Pre-Ship Reviews with Customer and Hardware Acceptance Reviews for deliveries.Planning of logistics, work instructions, hiring sub-contractors for shipment and handling of NASA Launch Abort System (LAS) – Successful launch of Pad Abort Test at WSMR.

Led streamlined design of Antares, Ground Support Equipment hardware which included increasing throughput for processing the fairing for Thermal Protection Systems.Developed Test Plans for Raceway to withstand Hot Fire Separation.Led team engineering efforts as KEI Stage 2 lead, during pathfinder at Vandenberg A.F.B., implemented designs, work packages, and drove non-conformances to closure. Lead Test engineer for GMD composite structures managing test teams and inspection.

Worked in various disciplines of Business Aviation related to Turbo Fan Engines, Thrust Reversers and Nacelles. Project and Test Engineer, Repair and Over Haul, FAR 25 and 33, Design and Configuration Management. Additional Experience on Valves and Air Management systems for Dassault and Hawker Horizon Programs.Qualified pneumatic valve hardware by gathering customer requirements, worked with the FAA representatives and tested to industry certification standards, wrote test procedures & similarity reports. Led and managed qualification tests at NTS and accomplished the test goals. (RTCA DO160) Completed Design for Six Sigma (DFSS), Green Belt Project - for variability of spring suppliers in common valve hardware.Led a Lean Velocity Project team to increase efficiencies with old drawing release system.Improved business processes by modifying engineering processes to utilize electronic system. Oversaw PLM (Product Life Management) data conversions to improve the customer use of the system, while maintaining export control and security.Supported Engine Test Programs for TFE 731-40, AS907 Engines/Nacelles and TF502/507.Worked with GKN suppliers to increase the quality of the Fan Cowl Door and Nacelle hardware by mandating processes to reduce redundant reworks and improved hardware receipt deadlines.Coordinated development between design and analysis teams for engine nacelle hardware and worked with local supplier for fast fabrication of FAR 25 and FAR 33 test hardware.

Worked as a Co-op Testing Material properties of plastics for Design. Worked on special projects to implement Specialized micro-beading for roto-molding processes.Ultrasonic welding, TnP Stress Cracking of Polycarbonates and Instron testing of components. Worked with a variety of Projects related to Design and Test of Plastic components and the associated thermal mold designs.