Abstract: We summarise the results of long-term research by these and other authors and propose engineering methods for fast optimisation of asteroid missions with planetary maneuvers near Venus, the Earth, Mars, Jupiter of various sequences and types. It permitted to reduce significantly characteristic velocity for reaching Main-belt asteroids having moderate orbital eccentricities and inclinations. The methods are simple and evident.Note: Research direction:Theoretical and applied problems of mechanic
The future interplanetary missions will probably use the conventional chemical rockets to leave the ...
The following paper presents the design of an optimal set of spacecraft formation orbits around an a...
This paper analyzes the feasibility of insertion of a 1000-metric ton asteroid into an Earth-Mars cy...
Abstract: We summarize the results of long-term by this and other authors and propose engi...
The future interplanetary missions will probably use the conventional chemical rockets to leave the ...
Abstract: The optimal trajectories of the spacecraft flight from the Earth to the Near-Ear...
Abstract: Optimal trajectories of the spacecraft from the Earth to near-Earth asteroid are...
Abstract: The solar electric propulsion could be the best option for the transports of the future du...
An indirect optimization method is applied to find rendezvous trajectories to reach asteroids of the...
Abstract: Optimal trajectories of a spacecraft flight to a near-Earth asteroid with using ...
The solar electric propulsion could be the best option for the transports of the future due to its h...
Abstract: Some methods of the asteroid hazard mitigation for the Earth using the missions ...
Abstract: This paper investigates spacecraft (SC) trajectories for the mission to a potent...
Abstract: Optimal trajectories of a spacecraft (S/C) flight to a near-Earth asteroid (NEA)...
Abstract: The purpose of this study is optimization of spacecraft flight to the Near-Earth...
The future interplanetary missions will probably use the conventional chemical rockets to leave the ...
The following paper presents the design of an optimal set of spacecraft formation orbits around an a...
This paper analyzes the feasibility of insertion of a 1000-metric ton asteroid into an Earth-Mars cy...
Abstract: We summarize the results of long-term by this and other authors and propose engi...
The future interplanetary missions will probably use the conventional chemical rockets to leave the ...
Abstract: The optimal trajectories of the spacecraft flight from the Earth to the Near-Ear...
Abstract: Optimal trajectories of the spacecraft from the Earth to near-Earth asteroid are...
Abstract: The solar electric propulsion could be the best option for the transports of the future du...
An indirect optimization method is applied to find rendezvous trajectories to reach asteroids of the...
Abstract: Optimal trajectories of a spacecraft flight to a near-Earth asteroid with using ...
The solar electric propulsion could be the best option for the transports of the future due to its h...
Abstract: Some methods of the asteroid hazard mitigation for the Earth using the missions ...
Abstract: This paper investigates spacecraft (SC) trajectories for the mission to a potent...
Abstract: Optimal trajectories of a spacecraft (S/C) flight to a near-Earth asteroid (NEA)...
Abstract: The purpose of this study is optimization of spacecraft flight to the Near-Earth...
The future interplanetary missions will probably use the conventional chemical rockets to leave the ...
The following paper presents the design of an optimal set of spacecraft formation orbits around an a...
This paper analyzes the feasibility of insertion of a 1000-metric ton asteroid into an Earth-Mars cy...