Jay Gounder Email & Phone Number

Bellevue, WA, US

Bellevue, Washington, US

Huntington Beach, California, US

Manage and lead the development efforts on state-of-the-art hypersonic missile technology.

Huntington Beach, California, US

Interface with multidisciplinary teams for design, analysis and test to provide life cycle engineering solutions and support. Plan and actualize test plans in accordance with programmatic requirements for advanced electromechanical systems. Manage environmental tests to qualify the tactical use of UAS Launcher Systems. Develop military standard test cable.

Huntington Beach, California, US

Orchestrate hardware fabrication, assembly and verification on 3-4 programs at any given time to meet schedule needs. Compose BOM, assembly and test procedures on a multitude of programs to maintain organization and effective direction. Integrate a non-lethal sUAS countermeasure with existing military UAS to protect civilians from collateral damage..

Arlington, VA, US

Oversee technical staff working on structural changes as the 787-10 transitioned from 74k lbf engines to 76k lbf engines. Implement preplanning and schedule preparation for all the structural analysis required for the engine transition. Perform resource forecasting and maintain record of the team’s time/effort spent to drive the development cost down.

Kent, WA, US

Model, construct and test a 2U satellite prototype for launch on the New Shepard launch vehicle and into sub-orbit on the Blue Origin New Shepard launch vehicle. Execute electrolysis of water in zero gravity to generate pressurized hydrogen and oxygen into tanks for a cubesat thruster. Program an onboard Raspberry Pi computer to conduct data collection of.

Continuous Rotating Detonation-Wave Engine LaboratoryPhotograph and produce well-defined Schlieren images. Provide constructive feedback regarding the recorded shock waves. Conduct gas chromatography and survey mixing results. Restructure, reconstruct and optimize engine plumbing.

Computational Plasma Dynamics LaboratoryCalculate thrust characteristics of the “ZaP Flow Z-Pinch Experiment” for advantageous plasma propulsion applications. Compute velocity and efficiency from measured mass, thrust, and specific impulse. Implement tabulated data on previous mars mission trajectories using STK and independently compose a refined.