Engineer

• Primary Support Cislunar and exploration-class orbital mechanics analysis and trajectory optimization
• Hypersonics, missiles, interceptors, and reentry vehicle trajectory design and optimization
• Time-dependent Traveling Salesman Problems and Facility Location Problem analysis
• Astrodynamics and orbital mechanics analysis including orbit propagation and maneuver design and optimization for orbit transfer, station keeping, graveyard, disposal, and reentry events
• Analysis of vehicles with chemical and/or electric propulsion
• Evaluating contested missions applications for space systems to understand threat performance, assess vulnerabilities, and improve system resiliency
• Developing Concepts of Operations (CONOPS), exploring Tactics, Techniques, and Procedures (TTPs), and incorporating operational constraints into the design and maturation of space and near-space systems
• Providing operational support for nominal launch and spacecraft deployment and transfer sequences, anomaly resolution, and on-call emerging events
• Utilizing optimal control, flight mechanics, and computer science/algorithm development skills to create new capabilities to service customer requests as stand-alone services and/or ready-to-integrate submodules
• Performing research and development and building new flight dynamics tools to cultivate and maintain a healthy and modern internal tool base
• Leveraging external tools like ASSET, GPOPS-II, SNOPT, POST, OTIS, Copernicus, GMAT, EMTG, etc. where appropriate to augment internally developed capabilities
• Additional inter-department partnership collaborations opportunities: Maneuver and orbit design, selection, and optimization for missions that support Rendezvous and Proximity Operations (RPO) objectives with complex operational constraints
• Trajectory design and optimization for launch vehicles and spacecraft for missions operating in LEO, MEO, HEO, GEO, and other earth-centric regimes

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