Abstract: We summarises the results of research by this and other authors concerning trajectories for asteroid missions and expeditions to larger Main Belt asteroids and trojan on missions dates time span in 1970-2030-s to reveal characteristic velocities and travel time dependence from the choice of maneuver dates and target asteroids. Unique simple methods of author proposed in earlier papers are used. Payload returning to the Earth is approximately calculated for some expeditions. These missions are supposed to be realisable.Note: Research direction:Theoretical and applied problems of mechanic
Different concepts for eliminating the threat of collision with a near-Earth object have been sugges...
Asteroids are becoming a stepping stone for the human space exploration,as much as they are a threat...
The problems of dynamics of celestial bodies are considered which in the literature are explained by...
Abstract: This paper investigates spacecraft (SC) trajectories for the mission to a potent...
Abstract: We summarise the results of long-term research by these and other authors and pr...
While standalone missions to the Trojan Asteroids of Mars are costly, we analyze flyby scenarios of ...
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: We summarize the results of long-term by this and other authors and propose engi...
Abstract: Trajectories of spacecraft with electro-rocket engine for missions to the Main B...
In simple terms, an asteroid retrieval mission envisages a spacecraft that rendezvous with an astero...
An indirect optimization method is applied to find rendezvous trajectories to reach asteroids of the...
There are hundreds of thousands of known asteroids, yet only 14 have been visited by spacecraft thus...
The present state of the knowledge of asteroids was assessed to identify mission and target prioriti...
Abstract: Some methods of the asteroid hazard mitigation for the Earth using the missions ...
Different concepts for eliminating the threat of collision with a near-Earth object have been sugges...
Asteroids are becoming a stepping stone for the human space exploration,as much as they are a threat...
The problems of dynamics of celestial bodies are considered which in the literature are explained by...
Abstract: This paper investigates spacecraft (SC) trajectories for the mission to a potent...
Abstract: We summarise the results of long-term research by these and other authors and pr...
While standalone missions to the Trojan Asteroids of Mars are costly, we analyze flyby scenarios of ...
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: We summarize the results of long-term by this and other authors and propose engi...
Abstract: Trajectories of spacecraft with electro-rocket engine for missions to the Main B...
In simple terms, an asteroid retrieval mission envisages a spacecraft that rendezvous with an astero...
An indirect optimization method is applied to find rendezvous trajectories to reach asteroids of the...
There are hundreds of thousands of known asteroids, yet only 14 have been visited by spacecraft thus...
The present state of the knowledge of asteroids was assessed to identify mission and target prioriti...
Abstract: Some methods of the asteroid hazard mitigation for the Earth using the missions ...
Different concepts for eliminating the threat of collision with a near-Earth object have been sugges...
Asteroids are becoming a stepping stone for the human space exploration,as much as they are a threat...
The problems of dynamics of celestial bodies are considered which in the literature are explained by...
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