Trajectories for the Sakigake extended-mission phaseThe trajectory profile that will be used by Japan's Sakigake spacecraft to accomplish its extended-mission objectives is described. Currently, Sakigake is following a heliocentric trajectory that will return to the earth's vicinity in January 1992. Four earth gravity-assist maneuvers are planned to redirect Sakigake to an encounter with Comet Honda-Mrkos-Pajdusakova (HMP) in February 1996. While carrying out the earth-swingby maneuvers, the spacecraft will make several passes through previously unexplored regions of the distant geomagnetic tail.
Document ID
19890050745
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Farquhar, R. (NASA Goddard Space Flight Center Greenbelt, MD, United States)
Dunham, D. (NASA Goddard Space Flight Center Greenbelt, MD, United States)
Hsu, S. (Computer Sciences Corp. El Segundo, CA, United States)
Uesugi, K. (NASA Goddard Space Flight Center Greenbelt, MD, United States)
Kawaguchi, J. (Institute of Space and Astronautical Science Sagamihara, Japan)
Date Acquired
August 14, 2013
Publication Date
January 1, 1988
Subject Category
Astrodynamics
Meeting Information
Meeting: International Symposium on Space Technology and Science