Acoustic Liner Design Utilizing Propagation Solvers of Varying Fidelity
Evaluating the Performance of Hybrid Vehicles between LEO, Cislunar Space, and Mars
Low-Thrust Transfers from Distant Retrograde Orbits to L2 Halo Orbits in the Earth-Moon System
Mars, Phobos, and Deimos Sample Return Enabled by ARRM Alternative Trade Study Spacecraft
Optimal orbits for sparse constellations of Mars navigation satellites
Optimum guidance for a low thrust interplanetary vehicle.
Sensitivity of the Asteroid Redirect Robotic Mission (ARRM) to Launch Date and Asteroid Stay Time
Simplified calculation of transition matrices for optimal navigation
Special orbits for the exploration of Mars and Venus