Flight Dynamics Engineer

Flight Dynamics Engineer

Requirements

• Bachelor’s degree in aeronautical/astronautical engineering, physics or applied mathematics, or related disciplines
• Eight or more years of experience in flight mechanics, astrodynamics, maneuver optimization, trajectory optimization, launch vehicle trajectory design, hypersonic vehicle modeling, or general trajectory modeling and simulation
• Proficiency in one or more of the following programming languages and environments: C, C++, Fortran, Python, Linux, and/or MATLAB
• The ability to operate independently, often in the presence of ambiguity, and still deliver high-quality, innovative, and specialized end products to a range of customers
• Willing to travel domestically approx. 10%
• The ability to obtain and maintain a US security clearance (TS clearance (SSBI) with SCI access) is required. U.S citizenship is required to obtain a security clearance
• Twelve or more years of experience of relevant technical work (for Senior Engineering Specialist)
• The ability to lead and execute large and sustained technical efforts with vision to propose, scope, and coordinate these efforts across organizational boundaries

Responsibilities

• Trajectory design and optimization for launch vehicles and spacecraft for missions operating in LEO, MEO, HEO, GEO, and other earth-centric regimes
• Astrodynamics and orbital mechanics analysis including orbit propagation and maneuver design and optimization for orbit transfer, stationkeeping, 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
• Exploring and defining the evolving Dynamic Space Operations (DSO) mission area
• Maneuver and orbit design, selection, and optimization for missions that support Rendezvous and Proximity Operations (RPO) objectives with complex operational constraints
• Developing Concepts of Operations (CONOPS), exploring Tactics, Techniques, and Procedures (TTPs), and incorporating operational constraints into the design and maturation of 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

Preferred Qualifications

• Advanced degree in aeronautical/astronautical engineering, physics or applied mathematics, or related disciplines is strongly desired
• Graduate level course work, research and/or experience in one or more of the following areas: orbital mechanics, astrodynamics, ascent trajectory modeling, hypersonic flight simulation, optimal control, flight mechanics, and/or trajectory modeling and simulation
• Experience using or building analysis software to combine numerical methods, orbital or flight mechanics, and optimization approaches for launch vehicles, missiles, interceptors, spacecraft, or reentry vehicles (hypersonics)
• Experience with nonlinear programming (non-linear programming), direct methods, gradient-based optimization, parameter optimization, genetic algorithms, evolutionary algorithms, heuristic optimization methods, indirect methods, and/or calculus of variations
• Advanced algorithm development skills to include parallel processing and scripting experience
• Experience with contested space trajectory applications, military exercises, and wargaming events
• Current TS (SSBI), TS/SCI, and/or TS/SAP Access