Infrastructure cybersecurity upgrades to facility related Industrial Control Systems.• Manage, organize, plan, direct and oversee day-to-day operational contract tasks/activities.• Manage expectations and relationships with the client senior management, company senior management and project teams.• Negotiate and oversee development, implementation and reporting of performance metrics.• Perform complete management and oversight functions for contract partners and subcontractors.• Provide technical team leadership for design, implementation, and installation.

Installation & Logistics (I&L), SETA government contractor, supporting, integrating, coordinating, reviewing, verifying and advising on various construction and demolition activities between the US Army Corp of Engineers (USACE) and vendor contractors.Completed modular trailer SCIF complex demolition project 2 months ahead of schedule.- Support Industrial Controls Systems (ICS) / Supervisory Control And Data Acquisition (SCADA) issues for operations building, power and chiller plants.- Support I&L Lien activities for lighting, electrical, maintenance, flooring, security doors, gas, HVAC, irrigation, and lightning protection systems.- Coordinate and generate Scheduled Maintenance Activities (SMAs) procedures for vendors.- Coordinate and schedule visitor access and escort requirements for visitors.

• Trajectory Team Lead for Atlas V NRO & Commercial launches (L-61, L-55, CLIO, L-39, and L-41), integrating Launch Vehicle Flight Design activities with customer, OSL, NRO, USAF, Aerospace Corporation, customer program office, engineering disciplines (guidance & navigation, control dynamics, flight software, thermodynamics and propulsion).• Chief analyst for Flight Design activities including trajectory optimization for launch and deployment of primary spacecraft (and secondary payloads), propellant margin analysis, RF Link analysis, Collision and Contamination Avoidance Maneuvers, Range Safety analysis, orbital lifetime analysis, upper stage de-orbit analysis, and post flight analysis.• Developed and coordinated ICD orbital and trajectory requirements with customer.• Flight Design Lead at Management Working Groups, Ascent Operations Working Groups, Integrated Management Reviews, Range, and at President Management Reviews.• Flight Design Lead in Integrated Crew Exercise and Mission Dress Rehearsals for launch.• Supported Vice President of Operations and Director of Recurring Operations for Day of Launch activities.• Flight Design Lead for Atlas and Delta IV&V working groups with USAF LR, CACI, Vencore, and the Aerospace Corporation.• Technical lead for trajectory simulation model updates, Simulation Data Book, and interface for trajectory design requirements from engineering disciplines including mass properties, guidance & navigation, flight software, control dynamics, thermodynamics, thermal and propulsion.• Flight Design Lead and coordinator with Propulsion for Atlas V SRB trajectory requirements, including ballistics, positioning, and statistical dispersion analysis.• Investigator for Delta II Corrective Action Boards during 2012-2013.• Participated in anomaly reviews in 2007, clearing Atlas V Flight Design for flight.• Programming analyst for Delta IV coordinates systems, mass properties and propulsion systems code conversions during 2012.

• Mission Engineer for final Atlas III (NROL-23) and first Atlas V NROL mission (NROL-30), integrated Launch Vehicle Flight Design activities with customer, OSL, NRO, USAF, Aerospace Corporation, customer program office, & engineering disciplines (guidance & navigation, control dynamics, flight software, thermodynamics and propulsion).• Chief Analyst for trajectory optimization for spacecraft launch and deployment, propellant margin, collision and contamination avoidance maneuvers, Injection Accuracy, Range Safety and post flight.• Developed and coordinated ICD trajectory requirements with customer.• Chaired Work Groups with customer, USAF, and Aerospace Corporation for Trajectory, Flight Controls, Aero-physics, Guidance & Navigation and Mass Properties.• Flight Design technical lead at Working Groups and major reviews.• Flight Lead for Day of Launch activities.• Provided performance trade studies, leading edge integration, and Basis of Estimate support for mission proposals for DSCS and NROL-34 missions.• Technical lead for trajectory simulation model updates, Atlas V Trajectory Simulation Data Book, and interface for trajectory design requirements from engineering disciplines including mass properties, guidance & navigation, flight software, control dynamics, aero-physics, loads, thermodynamics, thermal and propulsion.Trajectory Analyst for EELV Development 1997-2002• Provided trajectory performance studies of various Atlas V launch vehicle configurations. Developed and coordinated launch vehicle design and requirements with various systems engineering disciplines including mass properties, guidance & navigation, flight controls, loads & dynamics, aero-physics, structures, thermodynamics, thermal, propulsion and vehicle flight software.• Developed, coordinated and designed Atlas V Trajectory Simulation Data Book and Atlas Error Sources Documents.• Developed and maintained Atlas Flight Design / Mission Analysis website as webmaster.

Supervisor/Technical Lead Flight Mechanics Engineer Titan II Space Launch Vehicle (8/92 - 9/95) • Managed Flight Mechanics group assignments and technical analyses for Trajectory Design & Performance, Range Safety analysis, propellant margin analysis.• Flight Mechanics Work Group Chair.• DOL Winds Aloft analysis & coordination, and supported Titan IV DOL Work Groups. • Performed personnel evaluations and conducted employee appraisal reviews.• Responsible for Earned Value analysis as Flight Mechanics Cost Account Manager (CAM) for Titan II program.• Provided Basis of Estimate (BOEs) for Flight Mechanics Titan II proposals.• Co-authored MM White paper for Teledesic Corporation on System Design.• Product Integrity Engineer (PIE) - Responsible Engineer for Titan II Day-of-Launch (DOL) Procedures and Activities.• Product Integrity Engineer (PIE) –Responsible Engineer for Titan II Targeting Procedures and Activities analysis to support final Targeting Cycle for launch support.• Flight Mechanics technical lead for Titan II development program with solid strap on boosters.Primary Mission Engineer Titan II Launches (1988-1992)• Trajectory Analysis and Design, Performance Trade Studies, Range Safety Analyses, Propellant Margin Analyses, Synthetic Trajectory Analyses.• Supported Flight Mechanics Working Groups, Range Safety Working Groups, and Integration Management (ICD) Working Groups.

Aeromechanics & Loads Engineer, NSS Program (11/82-1/86)• Chief analyst for National Security Space (NSS) program as well as support to Titan IIIB, 34D and STS payloads. Responsibilities included ascent venting analysis and ground handling transportation loads of payloads, coordination with all engineering SC disciplines and systems, as well as ICD, PDR, and CDR support.• Supported design of Universal Payload Transporter to be used for ground, road and flight (C-5A) transport. • Assisted Primary SW Engineer with major upgrade of trajectory analysis code (FORTRAN IV/V).• Day of Launch (DOL) support included performing trajectory analysis of Titan launch vehicles for Winds Aloft Go/No Go criteria at Blue Cube (later named Onizucka, AFS). • Performed Wind Tunnel tests at Arnold Engineering Development Center and reduced data for initial assignments.• Performed aerodynamics drag analysis for ground structures, and F-16 antenna design.