Low-thrust Trajectory Capabilities for Exploration of the Solar System Using Nuclear Electric Propulsion
Low-thrust trajectory requirements for solar system exploration using nuclear electric propulsion
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Low-thrust trajectory requirements for solar system exploration using nuclear electric propulsion
Trajectory parameter determination in relation to various AROD airborne range and orbital determination ground stations
Two-variable asymptotic solution for three-dimensional solar powered low thrust trajectories in vicinity of ecliptic plane
General solutions to trajectory and orbit equations
Matched asymptotic expansion method applied to ordinary and optimal trajectory problems in hypervelocity flight dynamics
Periodic and almost periodic trajectories in cislunar space - techniques for determining behavior of dynamical systems of known periodic solutions, and space flight safety concept
Influence on trajectory determination of error in tracking station location and station time and frequency synchronization
Electric propulsion applied to lunar surface and Mars missions
Numerical calculation of three-dimensional trajectories using balanced horizontal and vertical motions
Numerical method for rocket trajectory determination from multistation Doppler tracking data
Conference on orbit and trajectory estimation
Mission, trajectory, and vehicle analyses of manned Mars stopover missions - advanced nuclear system parameters
Aerodynamic damping coefficient from wind tunnel free flight trajectories of nonaxisymmetrical bodies
Voyager mission study considerations including launch opportunities, trajectory design, performance capability of Saturn V launch vehicle, and vehicle load relief control
Optimal one- and two-impulse orbital transfer maneuvers, considering shallowly intersecting coplanar orbits
Flight path control in software system for Lunar Orbiter, discussing optimization program for midcourse aim point and lunar injection point
Science subsystems for Jupiter flyby missions, discussing equipment selection, mission planning, spacecraft design and trajectory and constraints on vehicle configuration
Mars stopover mission with Venus swingby technique, discussing velocity requirements, trip times and initial mass in earth orbit