Add to ORKGhonors thesisCollege of ScienceMathematicsElena CherkaevA new type of satellite transfer that uses half the amount of fuel as conventional transfers has been discovered. This transfer, called a low-energy transfer, proved to work in 1991 when a Japanese satellite successfully went in orbit around the moon using this technique. Since then, more research has been conducted to prove that a low-energy transfer can be accomplished between the moons of Jupiter. In the case of this current paper, it is shown that a low-energy transfer is possible from Earth to Mars using similar techniques as between the Jovian moons. This paper examines the existence of a low-energy transfer between the Earth and Mars. It begins by outlining the equilibrium point...
In 1991, the Japanese Hiten mission used a low energy transfer with a ballistic capture at the Moon ...
In this paper, a technique for the analysis and the design of low-energy interplanetary transfers, e...
The planar, circular, restricted three-body problem predicts the existence of periodic orbits around...
The use of CubeSats as space observation missions is now a reality. CubeSats are satellites in the c...
Techniques for low energy transfers have been applied to constructing trajectories to various locati...
The low-thrust version of the low energy transfers to the Moon exploiting the structure of the invar...
The low-thrust version of the low energy transfers to the Moon exploiting the structure of the invar...
This paper globally explores two-impulse, low-energy Earth–Moon transfers in the planar bicircular r...
Twenty years ago, the theoretical notions of low-energy transfers were put to test with the Japanese...
In this paper a technique based on the invariant manifolds theory has been optimized and applied to ...
The phenomenon by which a spacecraft can both approach a celestial body and start performing revolut...
In this paper novel Earth-Mars transfers are presented. These transfers exploit the natural dynamics...
In 1991, the Japanese Hiten mission used a low energy transfer with a ballistic capture at the Moon ...
In this paper, a technique for the analysis and the design of low-energy interplanetary transfers, e...
The planar, circular, restricted three-body problem predicts the existence of periodic orbits around...
The use of CubeSats as space observation missions is now a reality. CubeSats are satellites in the c...
Techniques for low energy transfers have been applied to constructing trajectories to various locati...
The low-thrust version of the low energy transfers to the Moon exploiting the structure of the invar...
The low-thrust version of the low energy transfers to the Moon exploiting the structure of the invar...
This paper globally explores two-impulse, low-energy Earth–Moon transfers in the planar bicircular r...
Twenty years ago, the theoretical notions of low-energy transfers were put to test with the Japanese...
In this paper a technique based on the invariant manifolds theory has been optimized and applied to ...
The phenomenon by which a spacecraft can both approach a celestial body and start performing revolut...
In this paper novel Earth-Mars transfers are presented. These transfers exploit the natural dynamics...
In 1991, the Japanese Hiten mission used a low energy transfer with a ballistic capture at the Moon ...
In this paper, a technique for the analysis and the design of low-energy interplanetary transfers, e...
The planar, circular, restricted three-body problem predicts the existence of periodic orbits around...