Analysis of Near Rectilinear Halo Orbit Insertion with a 40-kW Solar Electric Propulsion System
ON THE UTILITY OF THE MOON IN SPACE TRANSPORTATION- THE LUNATRON CONCEPT
A study of personnel propulsion devices for use in the vicinity of the moon, volume I
In-plane lunar injection opportunities from an orbiting space station
Cryogenic Propellant Management Device: Conceptual Design Study
Lunar Electromagnetic Launch System for In-Situ Resource Utilization
Analysis of Near Rectilinear Halo Orbit Insertion with a 40-kW Solar Electric Propulsion System
Linear Acceleration Guidance for Lunar Landing and Launch Trajectories