I founded Omnetix to solve a major industry challenge: getting key technologies to market and scale.We help leading companies bridge the gap between innovation and market success using a ‘Techonomics' approach, fusing technical and economic insights into ideal solutions.

Nonprofit dedicated to connecting space and terrestrial sectors for mutual benefit.

Developed a comprehensive debris removal architecture solution, leveraging refueling centered around debris clusters to lower the projected costs of Active Debris Removal by over 80%.Invented the Space Doughnut Model which balances the limits of the space environment with the needs of Earth; leveraged that to sculpt an incentive-based data sharing structure that promotes responsible and sustainable space growth.Developed financial sensitivity add-ons to UMPIRE to assess the driving cost factors in space refueling architecture optimization. Developed refueling case studies and UMPIRE features centered around the ability for various markets, such as LEO Earth Observation and GEO Telecommunications, to achieve economical retasking.Working on-orbit and ground fueling ConOps, requirements, and contingencies to inform product and systems architecture design.

Designed Orbit Fab's Shuttle-Depot refueling architecture through multi-disciplinary design practices resulting in a cost-effective refueling solution for a sustainable in-space economy.Led the design and development of UMPIRE feature development including training new team members to use the software and improve it.Invented the SUITE software which optimizes architectures for sustainable in-space and on-Earth resource utilization. SUITE stands for Symbiotic Universal ISRU Technology Engine.

Invented the UMPIRE software, which optimizes refueling architectures and ConOps for commercial and government customers. Leveraged this software to determine fuel pricing for the world's first in-space fuel sale. Used it to assess the feasibility of augmenting VLEO architectures with refueling. UMPIRE stands for Universal Mission Planner to Investigate Refueling Effectiveness.

Solved several orbital mechanics challenges regarding critical enabling methodologies for LEO refueling architectures. Performed docking kinematic analysis to inform on-orbit grappling interface designs. Developed electrical engineering test boards for spacecraft components.

Grew and lead the team from 30 to over 100 engineers in the design and development of the AggieSat6 Mission under funding from the University Nanosatellite Program and Air Force Research Laboratory. Resulted in being awarded flight selection and funding for the AggieSat6 mission!Created a number of additional projects all under the title AggieSat7, as well as a Research and Design class to successfully create a SmallSat Controls Testbed.

Responsible for leading the Thermal, Mechanisms, and Structures team to design, model, and test all related components and systems for the AggieSat 6 mission. AggieSat 6's mission was to design, deliver, and operate a pair of "listener" CubeSats that our organization proposed and developed with funding from the University Nanosatellite Program.

Worked under the Texas A&M University Center for Infrastructural Renewal to design a single-wheel test stand for terrain characterization via slippage and sinkage for AI pathfinding and trafficability in Space.

Researched, analyzed, and interactively modeled the accessibility of Lunar and Near Earth Asteroid resources (predominately water) as well as the needs of current orbital assets to propose the development of (eventually) self-sufficient in-space water supply chains.

Researched and developed analytics tools from scratch exploring the use of directed energy in space for propulsion (in thermal, ablative, and photonic modes), asteroid Ladar for planetary defense, economically viable power beaming, & more.