Add to ORKGA targeting scheme is presented to build trajectories from a specified Earth parking orbit to a specified low lunar orbit via a low-energy transfer and up to two maneuvers. The total transfer delta V (velocity) is characterized as a function of the Earth parking orbit inclination and the departure date for transfers to each given low lunar orbit. The transfer delta V (velocity) cost is characterized for transfers constructed to low lunar polar orbits with any longitude of ascending node and for transfers that arrive at the Moon at any given time during a month
Various Earth-Moon transfer trajectories are designed and analyzed to prepare the future Korea's Lun...
Twenty years ago, the theoretical notions of low-energy transfers were put to test with the Japanese...
Techniques for low energy transfers have been applied to constructing trajectories to various locati...
Recent lunar missions have begun to take advantage of the benefits of low-energy ballistic transfers...
This study demonstrates how to use dynamical systemsmethods to construct families of low-energy ball...
Low-energy transfers utilizing multi-body dynamics show great promise for future space exploration; ...
: In the frame of the lunar exploration, numerous future space mis-sions will require maximization o...
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...
A search for low Δ V Earth-to-Moon trajectories has been initiated. Numerical integration of the equ...
In the Earth-Moon system, low-energy orbits are transfer trajectories from the earth to a circumluna...
This paper deals with the design and optimization of transfer trajectories from the Earth to the Moo...
The use of CubeSats as space observation missions is now a reality. CubeSats are satellites in the c...
Secondary payloads have a rich and successful history of utilizing cheap rides to orbit to perform o...
Mission design requires the efficient management of spacecraft fuel to reduce mission cost, increase...
Various Earth-Moon transfer trajectories are designed and analyzed to prepare the future Korea's Lun...
Twenty years ago, the theoretical notions of low-energy transfers were put to test with the Japanese...
Techniques for low energy transfers have been applied to constructing trajectories to various locati...
Recent lunar missions have begun to take advantage of the benefits of low-energy ballistic transfers...
This study demonstrates how to use dynamical systemsmethods to construct families of low-energy ball...
Low-energy transfers utilizing multi-body dynamics show great promise for future space exploration; ...
: In the frame of the lunar exploration, numerous future space mis-sions will require maximization o...
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...
A search for low Δ V Earth-to-Moon trajectories has been initiated. Numerical integration of the equ...
In the Earth-Moon system, low-energy orbits are transfer trajectories from the earth to a circumluna...
This paper deals with the design and optimization of transfer trajectories from the Earth to the Moo...
The use of CubeSats as space observation missions is now a reality. CubeSats are satellites in the c...
Secondary payloads have a rich and successful history of utilizing cheap rides to orbit to perform o...
Mission design requires the efficient management of spacecraft fuel to reduce mission cost, increase...
Various Earth-Moon transfer trajectories are designed and analyzed to prepare the future Korea's Lun...
Twenty years ago, the theoretical notions of low-energy transfers were put to test with the Japanese...
Techniques for low energy transfers have been applied to constructing trajectories to various locati...