Physics
Scientific paper
Apr 2003
adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=2003adspr..31.2005w&link_type=abstract
Advances in Space Research, Volume 31, Issue 8, p. 2005-2010.
Physics
1
Scientific paper
Artificial satellites around the Earth can be temporarily captured by the Moon via gravitational mechanisms. How long the capture remains depends on the phase space region where the trajectory is located. This interval of time (capture time) ranges from less than one day (a single passage), up to 500 days, or even more. Orbits of longer times might be very useful for certain types of missions. The advantage of the ballistic capture is to save fuel consumption in an orbit transference from around the Earth to around the Moon. Some of the impulse needed in the transference is saved by the use of the gravitational forces involved. However, the time needed for the transference is elongated from days to months. In the present work we have mapped a significant part of the phase space of the Earth-Moon system, determining the length of the capture times and the origin of the trajectory, if it comes from the Earth direction, or from the opposite direction. Using such map we present a set of missions considering the utilization of the long capture times.
Cabo Winter Othon
Prado Antonio F. Bertachini A.
Vieira Neto Ernesto
No associations
LandOfFree
Orbital maneuvers using gravitational capture times does not yet have a rating. At this time, there are no reviews or comments for this scientific paper.
If you have personal experience with Orbital maneuvers using gravitational capture times, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Orbital maneuvers using gravitational capture times will most certainly appreciate the feedback.
Profile ID: LFWR-SCP-O-919074