I have over 17 years of relevant experience in a testing and engineering environment dating back to the mid-2000s when I was working for a Curtiss-Wright group on nuclear power plant safety components and have worked on some major NASA projects in the past few years as a subject expert in a few technical areas and manufacturing processing.
The most resent project I worked was a joint Space Force, NASA, and FAA managed project as part of Lox Methane Assessment at MSFC as a test engineer. Some things I did during this time, I designed a 25lb test article that Mixed Liquid Methane and Liquid Oxygen to form a Liquid High Explosive know as MOX, review and wrote testing CONOPS, Hazard analysis, and part of other engineering reviews for 100 lb Confine by Missile test that will be performed at Redstone Test Area this year. Prior to that I was a NASA Civil Servant and carried out duties such HLS Cryofluid Management technical representative for the NASA integration team while on the NASA HLS insight team, I also work on several programs related to NASA NTP efforts and small green propellant satellites utilizing liquid high explosive propellants such as AF-315E. Further back I worked on Supporting efforts at MSFC in advance concepts such as Pulsed nuclear fission fusion (PuFF) propulsion system that is mini version of the old Orion utilize high voltage pulse power systems to initiate a confined nuclear explosion in a nozzle to generate thrust. As part of that project, I lead testing efforts in the field of pulse power development and low jitter high speed triggering of high voltage systems. I have also worked on testing and instrumentation for various projects using Oscilloscope, Time Domain Reflectometer, and NI Labview hardware. Also started and ran a small business that dealt with various mil spec and government standards for over a decade.
During the past I have been part of multiple group achievement awards for projects such as Pulse Fission Fusion (PuFF) at MSFC and various Cryogenic Awards Projects across MSFC and GRC.