Develop spacecraft descent GNC algorithms, sensor models, and navigation systems, using C/C++ and Python. Evaluate performance, support closed-loop and system-level testing, and apply failure mode analysis.
About this role
This senior engineering role sits within the JP Engineering CTO Office and supports lunar missions through mission analysis and flight dynamics. The work focuses on spacecraft trajectory design, mission performance, correction maneuvers, and operational planning for lunar flight activities.
The engineer will analyze and optimize trajectories, generate launch windows, perform covariance analysis, and develop and maintain in-house astrodynamics libraries. The role also covers mission requirements traceability, verification and validation, process improvement, and support for Orbit Determination and Maneuver Planning. Required qualifications include at least five years of mission analysis experience on cislunar or deep-space missions, professional experience with orbital mechanics tools such as GMAT, STK, MONTE, Orekit, or similar, and professional software development experience involving testing, version control, and Dockerized environments. Familiarity with CR3BP, covariance analysis, Lambert transfers, or B-plane targeting is also required.
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