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Completed TRL 3 (started at 2, targeting 3)
This work will develop models and simulation capabilities to parametrically assess position, navigation, and timing capabilities of the next-gen Mars relay. Alternate orbits and constellation approaches for the hybrid architecture (low-altitude repeaters with high-altitude ‘trunk-line’ orbiters) and monolithic constellations will be explored.
Including the impacts of navigation to a constellation design, in addition to communication and data volumes that are currently considered, can both impact the optimality of a given design and reduce the need for Earth-based tracking. Using navigation derived from links between spacecraft creates the opportunity for autonomous navigation, increased accuracy, fault tolerance, enabling for power-limited spacecraft, and decreased DSN loading
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