Add to ORKGComputer program for electric propelled spacecraft interplanetary, flyby, and rendezvous trajectory ...
Low-thrust electric propulsion provides many advantages for mission to difficult targets-Comets and ...
This research describes a prototype software navigation system that would allow a spacecraft with a ...
Computer program has been designed to handle computations for low thrust missions rapidly and with a...
Trajectory and spacecraft design data for unmanned interplanetary missions using suboptimal powered ...
A performance-analysis computer program, that was developed explicitly to generate optimum electric ...
AAS/AIAA Astrodynamics Specialist Conference Big Sky, MT, August 3 - 7, 2003.A multipurpose low thr...
Recent interest at NASA for the application of solar electric propulsion for the transfer of signifi...
Minimum propellant consumption trajectories to Mars for constant-thrust, constant-specific impulse v...
A simple family of indirect transfer trajectories between circular orbits is used to evaluate the ma...
An interplanetary low-thrust, solar electric propulsion mission simulation program suitable for navi...
A trajectory-optimization process is described in which the optimum thrust equations are derived usi...
Upon completion of the heliocentric leg of its mission, it is almost always the case that an interpl...
A tool developed for the preliminary design of low-thrust trajectories is described. The trajectory ...
Computer programs for solving trajectory and system optimization problems of electrically propelled ...
Computer program for electric propelled spacecraft interplanetary, flyby, and rendezvous trajectory ...
Low-thrust electric propulsion provides many advantages for mission to difficult targets-Comets and ...
This research describes a prototype software navigation system that would allow a spacecraft with a ...
Computer program has been designed to handle computations for low thrust missions rapidly and with a...
Trajectory and spacecraft design data for unmanned interplanetary missions using suboptimal powered ...
A performance-analysis computer program, that was developed explicitly to generate optimum electric ...
AAS/AIAA Astrodynamics Specialist Conference Big Sky, MT, August 3 - 7, 2003.A multipurpose low thr...
Recent interest at NASA for the application of solar electric propulsion for the transfer of signifi...
Minimum propellant consumption trajectories to Mars for constant-thrust, constant-specific impulse v...
A simple family of indirect transfer trajectories between circular orbits is used to evaluate the ma...
An interplanetary low-thrust, solar electric propulsion mission simulation program suitable for navi...
A trajectory-optimization process is described in which the optimum thrust equations are derived usi...
Upon completion of the heliocentric leg of its mission, it is almost always the case that an interpl...
A tool developed for the preliminary design of low-thrust trajectories is described. The trajectory ...
Computer programs for solving trajectory and system optimization problems of electrically propelled ...
Computer program for electric propelled spacecraft interplanetary, flyby, and rendezvous trajectory ...
Low-thrust electric propulsion provides many advantages for mission to difficult targets-Comets and ...
This research describes a prototype software navigation system that would allow a spacecraft with a ...