A Tisserand-Based Reachability Criterion for Gravity-Assist Selection: Why a Single Venus Flyby Is Ineffective for Rendezvous with (16) Psyche
Jorge Nisperuza, Sebastian Valencia, Randy CastilloThis study investigates why single planetary gravity assists fail to provide competitive impulsive architectures for rendezvous with the metallic main-belt asteroid (16) Psyche. A decade-long Lambert-based trajectory survey (2028–2037) is performed using a patched-conic model with powered gravity assists to compare direct Earth–Psyche, Earth–Mars–Psyche, and Earth–Venus–Psyche transfer architectures. The optimal direct transfer requires 9.65 km s−1, whereas Venus-assisted trajectories demand 15.3–15.7 km s−1. For Mars, the survey shows that no feasible near-ballistic solution exists within the entire decade: the low-energy Earth–Mars legs arrive at Mars with the hyperbolic excess velocity directed against the planet’s motion, so that redirecting it towards the asteroid belt requires turn angles of approximately 115–120°, far exceeding the ≈65° that Mars can deliver at its minimum allowable flyby periapsis, defined as the planetary mean radius plus a 250 km altitude margin. Two complementary analytical results explain this behaviour. A Tisserand-based reachability criterion shows that reaching Psyche requires a minimum hyperbolic excess speed of approximately 9.8 km s−1 at Venus but only 4.1 km s−1 at Mars, an energetic penalty that is fixed before the encounter because an unpowered flyby preserves the magnitude of the excess velocity. A directional feasibility condition then shows that satisfying the scalar criterion is necessary but not sufficient: the excess-velocity vector delivered by the inbound leg must also lie within the attainable deflection cone of the assisting planet, a condition that Venus fails energetically and Mars fails geometrically. Together, the two conditions form a predictive analytical framework for screening gravity-assist planets prior to computationally intensive optimisation, and they explain why low-thrust propulsion—rather than any single impulsive flyby—underpins the trajectory of NASA’s Psyche mission.