Senior astrodynamics engineer analyzing orbital dynamics and designing optimized spacecraft trajectories. Using STK, Python, and MATLAB to support advanced space missions.
Responsibilities
Perform advanced orbit dynamics and astrodynamics analysis for space missions
Conduct spacecraft trajectory design and optimization
Apply advanced orbital mechanics and perturbation theory to mission analysis
Perform orbit determination and estimation analysis
Evaluate and optimize mission trajectories using analytical and computational methods
Conduct mission design and architecture analyses across a range of mission scenarios
Utilize Systems Tool Kit (STK) extensively for mission analysis and simulation
Apply STK modules including Astrogator, Optimizer, Coverage, and Communications
Develop STK automation and scripting solutions using APIs and STK Connect
Build and maintain mission analysis models and simulations to support technical decision-making
Develop advanced engineering analysis tools, models, and simulations using Python and MATLAB
Apply computational methods to solve complex astrodynamics and mission analysis problems
Support software development practices, including version control, testing, documentation, and CI/CD
Lead complex technical analyses and engineering investigations
Conduct multidisciplinary trade studies evaluating mission architectures and technical alternatives
Independently identify, analyze, and solve challenging astrodynamics problems
Present technical findings, recommendations, and analysis results to engineering stakeholders
Contribute technical expertise to mission design decisions and program development
Requirements
Must be legally eligible to work in Canada
Must be capable of obtaining the required security clearance
Must be willing to work at least 50% on-site in Montreal
Strong written and verbal communication skills in English required
Master's degree in Aerospace Engineering, Astronautical Engineering, Physics, Applied Mathematics, or a closely related field
Bachelor's degree with significant additional relevant experience, typically 9+ years, will also be considered
Minimum 7 years of professional post-graduation experience directly related to orbit dynamics, astrodynamics, trajectory optimization, and space mission design and analysis
Expert-level proficiency with STK, including Astrogator, Optimizer, Coverage, and Communications
Demonstrated experience with STK automation and scripting, including API and STK Connect
Advanced programming proficiency in Python and MATLAB, with experience developing engineering analysis tools, models, or simulations
In-depth theoretical and practical knowledge of advanced orbital mechanics, perturbation theory, orbit determination and estimation, trajectory optimization, gradient-based optimization methods, and evolutionary optimization methods
Proven ability to independently lead technical analyses and complex trade studies
Excellent analytical, critical-thinking, and problem-solving skills
Ph.D. in Aerospace Engineering or a closely related field with a focus on astrodynamics or orbital mechanics (preferred)
Experience with GMAT, FreeFlyer, Orekit, or SPICE (preferred)
Experience with C/C++ programming (preferred)
Experience with spacecraft Guidance, Navigation, and Control (GNC) analysis or design (preferred)
Experience with multi-body dynamics (preferred)
Experience supporting large satellite constellations (preferred)
Experience with satellite operations, particularly flight dynamics activities (preferred)
Experience with software development best practices, including Git, software testing, technical documentation, and CI/CD (preferred)
Publications or conference presentations in astrodynamics, orbital mechanics, or related fields (preferred)
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