A novel slow push asteroid deflection strategy has been recently proposed in which an Earth threatening asteroid can be deflected by exploiting the momentum transmitted by a collimated beam of quasi-neutral plasma impinging against the asteroid surface. The beam can be generated with state-of-the art ion engines from a hovering spacecraft with no need for physical attachment or gravitational interaction with the celestial body. The spacecraft, placed at a distance of a few asteroid diameters, would need an ion thruster pointed at the asteroid surface as well as a second propulsion system to compensate for the ion engine reaction and keep the distance between the asteroid and the shepherd satellite constant throughout the deflection phase. A...
The Asteroid Tugboat (AT) is a fully controlled asteroid deflection concept using a robotic spacecra...
We assess in this paper 3 different deflection approaches for a wide range of virtual collision scen...
In this paper we assess and compare the effectiveness of four classes of non-nuclear asteroid deflec...
The Ion Beam Deflection provides the following potential advantages over other asteroid deflection s...
Mission scenarios for the deflection of fictitious asteroid 2017 PDC are investigated. Two deflectio...
Mission scenarios for the deflection of fictitious asteroid 2017 PDC are investigated. Two deflectio...
Mission scenarios for the deflection of fictitious asteroid 2017 PDC are investigated. Two deflectio...
Mission scenarios for the deflection of fictitious asteroid 2017 PDC are investigated. Two deflectio...
Mission scenarios for the deflection of fictitious asteroid 2017 PDC are investigated. Two deflectio...
Mission scenarios for the deflection of fictitious asteroid 2017 PDC are investigated. Two deflectio...
This paper presents a novel idea for the successful deflection of asteroids. Adapted initially from ...
This paper presents a novel idea for the successful deflection of asteroids. Adapted initially from ...
Automated surveys along with population models have determined that tens of thousands Near Earth Obj...
The near-Earth object population, composed mostly of asteroids rather than comets, poses an impact h...
The Gravity Tractor (GT) is a fully controlled asteroid deflection concept using the mutual gravity ...
The Asteroid Tugboat (AT) is a fully controlled asteroid deflection concept using a robotic spacecra...
We assess in this paper 3 different deflection approaches for a wide range of virtual collision scen...
In this paper we assess and compare the effectiveness of four classes of non-nuclear asteroid deflec...
The Ion Beam Deflection provides the following potential advantages over other asteroid deflection s...
Mission scenarios for the deflection of fictitious asteroid 2017 PDC are investigated. Two deflectio...
Mission scenarios for the deflection of fictitious asteroid 2017 PDC are investigated. Two deflectio...
Mission scenarios for the deflection of fictitious asteroid 2017 PDC are investigated. Two deflectio...
Mission scenarios for the deflection of fictitious asteroid 2017 PDC are investigated. Two deflectio...
Mission scenarios for the deflection of fictitious asteroid 2017 PDC are investigated. Two deflectio...
Mission scenarios for the deflection of fictitious asteroid 2017 PDC are investigated. Two deflectio...
This paper presents a novel idea for the successful deflection of asteroids. Adapted initially from ...
This paper presents a novel idea for the successful deflection of asteroids. Adapted initially from ...
Automated surveys along with population models have determined that tens of thousands Near Earth Obj...
The near-Earth object population, composed mostly of asteroids rather than comets, poses an impact h...
The Gravity Tractor (GT) is a fully controlled asteroid deflection concept using the mutual gravity ...
The Asteroid Tugboat (AT) is a fully controlled asteroid deflection concept using a robotic spacecra...
We assess in this paper 3 different deflection approaches for a wide range of virtual collision scen...
In this paper we assess and compare the effectiveness of four classes of non-nuclear asteroid deflec...