2027 Multi-Domain Trajectory Design Engineer

Job description

The Aerospace Corporation is the trusted partner to the nation’s space programs, solving the hardest problems and providing unmatched technical expertise. As the operator of a federally funded research and development center (FFRDC), we are broadly engaged across all aspects of space— delivering innovative solutions that span satellite, launch, ground, and cyber systems for defense, civil and commercial customers. When you join our team, you’ll be part of a special collection of problem solvers, thought leaders, and innovators. Join us and take your place in space. Job Description The Enterprise Effects Division (EED) drives integration of Aerospace’s strategic capabilities across the national space enterprise. The division leverages a broad array of engineering disciplines against a diverse and dynamic portfolio of programs, customers, and national challenges. EED spans the capability lifecycle from concept and architecture design to performance assessment to application of space and space-enabled capabilities. As a core component of EED, the Emerging Missions Flight Dynamics Department (EMFDD) provides flight mechanics expertise for the cislunar domain, multi-objective “traveling salesman” trajectory sequence generation, facility location optimization, and trans-atmospheric flight design for missiles, hyperglide vehicles, and reentry vehicles. Relevant skills include orbital mechanics, astrodynamics, trajectory design and optimization, and atmospheric flight modeling and simulation. The selected candidate will provide expertise for a wide range of customer flight mechanics needs, supporting analysis, research, and development requests. The work will require candidates to provide deep technical solutions while also collaborating with engineering partners to facilitate integrated solutions for our customers’ hardest problems. Customers will include defense, intelligence, and civil and commercial organizations. Work Model This is a full-time position based in El Segundo, CA, Huntsville, AL, or Albuquerque, NM, offering an in-person work model that combines 4 or more regular onsite workdays per week and remote flexibility as business needs allow. What You’ll be Doing: Primary Support Trajectory design and optimization for hypersonic/high-speed systems, missiles, interceptors, and reentry vehicles Missile system and missile defense engagement simulation and performance analysis Multi-domain mission design for systems transiting orbital and atmospheric regimes Constrained optimal control determination for vehicles with aerodynamic and/or propulsive forces (chemical, electric, other) Contested space mission evaluation: threat assessment, vulnerability analysis, and system resiliency improvement CONOPS development, TTP exploration, and operational constraint integration for space, near-space, and reentry systems Development of new capabilities using optimal control, flight mechanics, and algorithm development for stand-alone services and integration-ready submodules Algorithm and software R&D to maintain modern internal tool base Application of external tools like ASSET, GPOPS-II, SNOPT, POST, OTIS, Copernicus, GMAT, EMTG, etc. where appropriate to augment internally developed capabilities Additional support opportunities: Cislunar and exploration-class trajectory optimization and application of dynamical systems theory Time-dependent Traveling Salesman Problems and Facility Location Problem analysis Reentry risk and range safety assessments Astrodynamics analysis: orbit propagation, maneuver design/optimization for orbit transfer, station keeping, graveyard, disposal, and reentry Operational support for nominal launch, spacecraft deployment/transfer, anomaly resolution, and emerging events Maneuver and orbit design/optimization for Rendezvous and Proximity Operations (RPO) with complex constraints Trajectory design and optimization for launch vehicles and spacecraft for missions operating in LEO, MEO, HEO, GEO, and other earth-centric regimes What You Need to be Successful Minimum Requirements for Member of Technical Staff – Flight Mechanics: Master’s degree from an accredited college/university program in Engineering, Science, Mathematics, or related technical discipline (pursuing or conferred within last 12 months) 0-1 years of relevant professional, technical work experience. Experience in one or more of the following subjects: space mission analysis and design, advanced astrodynamics, algorithm design, software development, or mathematical modeling, multi-objective optimization, trajectory simulation and performance optimization of spacecraft, missiles, and reentry vehicles Proficiency with one or more of the following programming languages/tools: C, C++, Python, Fortran, MATLAB. Effective written and verbal communication skills. Willing to travel domestically to customer and contractor facilities (approx. 10%) This position requires the ability to obtain and maintain a security clearance, which is issued by the US government. U.S citizenship is required to obtain a security clearance. In addition to the above, the minimum requirements for Senior Member of Technical Staff – Flight Mechanics position include: Ph.D. from an accredited college/university program in Engineering, Science, Mathematics, or related technical discipline (pursuing or conferred within last 12 months) 0-1 year of iof relevant professional, technical work experience. Demonstrated technical excellence in the relevant job capabilities and functions The ability to operate independently, often in the presence of ambiguity, and still deliver high quality, relevant end products to a range of customers How You Can Stand Out It would be impressive if you have one or more of these: Research or professional experience in engineering, mathematics, physics, computer science, or related field. Experience using or building analysis software to combine numerical methods, orbital or flight mechanics, and optimization approaches for l