This paper presents two conceptual designs of multi-spacecraft swarms used for deflecting Apophis. Each spacecraft is equipped with a solar concentrator assembly, which focuses the solar light, and a beaming system that projects a beam of light onto the surface of the asteroid. When the beams from each spacecraft are superimposed, the temperature on the surface is enough to sublimate the rock, creating a debris plume with enough force to slowly alter the orbit of Apophis. An overview of the dynamics, control and navigation strategies are presented along with preliminary system budgets
In 1993 solar concentrators were first proposed to deflect asteroids away from a collision course wi...
In 1993 solar concentrators were first proposed to deflect asteroids away from a collision course wi...
A solution to the asteroid deviation problem via a low-thrust strategy is proposed. This formulation...
This paper presents two conceptual designs of multi-spacecraft swarms used for deflecting Apophis. E...
This paper presents some recent results on the deflection of potentially dangerous Near Earth Object...
This paper presents some recent results on the deflection of potentially dangerous near earth object...
This paper presents the conceptual design of multiple spacecraft system for the use of deflecting Ne...
Two strategies are presented for the positioning and control of a spacecraft formation designed to f...
This paper presents an analysis of an asteroid deflection method based on multiple solar concentrato...
This purpose of this dissertation is to ascertain whether solar sublimation is a viable method for t...
This purpose of this dissertation is to ascertain whether solar sublimation is a viable method for t...
A solution to the asteroid deviation problem via a low-thrust strategy is proposed. This formulation...
A solution to the asteroid deviation problem via a low-thrust strategy is proposed. This formulation...
Since the first Near Earth Object (NEO) defence system, Project Icarus, was published in 1967, where...
In 1993 solar concentrators were first proposed to deflect asteroids away from a collision course wi...
In 1993 solar concentrators were first proposed to deflect asteroids away from a collision course wi...
In 1993 solar concentrators were first proposed to deflect asteroids away from a collision course wi...
A solution to the asteroid deviation problem via a low-thrust strategy is proposed. This formulation...
This paper presents two conceptual designs of multi-spacecraft swarms used for deflecting Apophis. E...
This paper presents some recent results on the deflection of potentially dangerous Near Earth Object...
This paper presents some recent results on the deflection of potentially dangerous near earth object...
This paper presents the conceptual design of multiple spacecraft system for the use of deflecting Ne...
Two strategies are presented for the positioning and control of a spacecraft formation designed to f...
This paper presents an analysis of an asteroid deflection method based on multiple solar concentrato...
This purpose of this dissertation is to ascertain whether solar sublimation is a viable method for t...
This purpose of this dissertation is to ascertain whether solar sublimation is a viable method for t...
A solution to the asteroid deviation problem via a low-thrust strategy is proposed. This formulation...
A solution to the asteroid deviation problem via a low-thrust strategy is proposed. This formulation...
Since the first Near Earth Object (NEO) defence system, Project Icarus, was published in 1967, where...
In 1993 solar concentrators were first proposed to deflect asteroids away from a collision course wi...
In 1993 solar concentrators were first proposed to deflect asteroids away from a collision course wi...
In 1993 solar concentrators were first proposed to deflect asteroids away from a collision course wi...
A solution to the asteroid deviation problem via a low-thrust strategy is proposed. This formulation...