• Developing all weather drone platforms that far surpass capabilities of current quadcopter drones within its size/weight class. These new drone platforms have multiple use cases & applications• Developing drone based platform used to clean windows of tall buildings and vertical surfaces• EIA Award Winner – April 2019.• Selected for prestigious UCONN TIP Program

• Founded company and developed business model based on need for low cost custom web development for resorts in popular vacation areas. • Lead small team to build and designed over 100 websites for primarily hotels and resorts throughout the USA & Caribbean.• Coded with HTML, CSS, Javascript & PHP used custom code within the Wordpress platform providing each and every client with a unique design that reflect their resorts• Responsible for all sales & new business development. Successfully cold called and gathered now over 100 clients.• Work with clients post launch to provide marketing services, primarily utilizing Google Adwords with online booking/conversion tracking to produce an ROI for each hotel client every month

• Head of New Product Development – Designed and developed multiple kiosks from conception, to prototype to production including: VengoXL, Countertop Unit, Vengo Vehicle Model, Card Dispenser & In-Aisle machineShark Tank March 2017• Pitched Vengo Mini Compact High Tech Vending machine, alongside co-founder Brian Shimmerlik on NBC’s Shark Tank. • Engineering Team Lead. Responsible for weekly coordination meetings & hardware and software team direction. • Designed all mechanical components of Vengo tech min compact vending machine units from conceptual stage all the way to detail design.• Responsible for Supply Chain Management of all metal, plastics & standard parts, work with multiple suppliers on an almost daily basis.• Coordinate logistics of Vengo’s restocking operations• Set up framework for Vengo Product testing to achieve 99% product vending reliability.

Lead Mechanical Design Engineer for Propulsion Team – S-97 Raider Program • Responsible for layout of APU (Auxiliary Power Unit) and ECS (Environmental Control System), including all the ducting, from conceptual to PDR phase• Responsible for layout of aircraft Bleed Air System, from mid-conceptual to PDR phase• Responsible for main engine build up design including design of main engine support mounts, all engine and engine bay drain lines, IPS duct, and engine to engine intake flex bellow.• Designed NACA cooling inlets for S-97 main engine bay • Designed cooling inlets/scoops and screens for S-97 avionics cooling along with all main avionics cooling ducting• Responsible for design of S-97 Fuel Bladder and entire S-97 Fuel System layout, from conceptual design to post PDR phase/present day. This includes Fuel qty gauging, bladder fittings and access panels, vent lines and vent fittings, fuel bladder maneuvering can, bladder mounting, and internal and external fuel lines for entire fuel system.• Responsible for layout of aircraft Fire Suppression System, from mid-conceptual to post PDR phase/present day• Helped line up suppliers for components for all systems mentioned above. Continue to work almost daily with suppliers for main engine, fuel, APU, ECS, and Avionics cooling systems.Patent File # ID-0018215-US - Sleeve Rod for Hanging Fuel BladderPatent filed for simple method to mount the fuel bladder between two structural keels. Driving issue was accessibility to the S-97 Raider fuel bladder. General Design Use CATIA V5 CPD (Composite Product Definition) to design ply layers and lay-up for APU Inlet Duct for S-92 AES (Advanced Exhaust System)Designed and released Mod Package for Fuel Jettison Modification to S-92 Helicopter.Reviewed manufacturing issues on Blackhawk and Medevac helicopters and generated ECs (Engineering Changes) when necessary.

• Founded web development company with friend/business partner in 2008.• Responsible for a wide variety of tasks on all projects from site conception to completion• Lead/Sole front-end developer for all Scratch’s websites• Back-end developer for most of Scratch’s websites.• Estimates time needed for project proposals and project plans• Participates in prospective client meetings/telecoms and works directly with all clients• Coordinates with designers and clientsFRONT END LEAD/SOLE DEVELOPER:Flexmg.comKevinKalikow.comNewschool.edu/Milano/nycaffairs/Strongman.comSunpill.com

Responsible for mechanical design of entire AW129 BCH composite Engine Intake, including all sub assemblies and hardware.Responsible for 95% of all drawings associated with the AW 129 BCH program from start to finish. This includes detail parts, sub-assemblies, major assemblies, tooling drawings and customer interface drawings.Use CATIA V5 to design heated composite inlet and bulkheads for AW129 BCH Intake.Designed tooling fixtures, specifically complete trim and drill fixtures for both Inner Duct halves of AW129 BCH Engine Intake. Oversaw build and physically assembled fixtures to ensure accuracy.Imported modeled machines parts, such as bulkheads and trim and drill fixtures, in correct file into PROCAM software for proper CNC machiningResponsible for monthly weight analysis of programExperience designing full scale and scale SLA prototype models

Responsible for all design changes of all GA-ASI aircraft pylons.Use Pro-Engineer to design composite structural components for the Predator-B Unmanned Aerial Vehicle. Responsible for complete design of new upgraded Predator-B intake ducts.Implemented composite prototype upgrades to full scale production parts for the Predator-B.

Use CATIA V5 to design composite skins, bulkheads, and frames for the Sikorsky CH-53K Super Stallion Utilize Enovia V5 LCA (Product Lifecycle Management tool) for preliminary design.

Use CATIA V5 & FiberSim to design composite skins & straps for the Joint Strike Fighter. Experience designing broad variety of composites including: permanent composite skins, removable composite doors & panels, composites with honeycomb core as well as SynCore, and composites with complex curvature and rough/non-tangential surfaces.Experience designing composite skin assemblies including removable panels with attached titanium screens & stiffeners.Responsible for design of majority of CV

Redesigned components for the Multiple Launch Rocket System. Performed numerous tolerance analyses on interfaces for the M270 and M270A1 elevation actuator.Updated and accurately represented M270 and M270A1 Pro-E files into the Pro-Interlink Database.