Inclination Change Efficiency: A Geocentric Orbit Transfer Guidance Method Using Continuous Low Thrust
Spacefight mechanics conference; 6th, Spaceflight mechanics 1996 ; 1996 ; Austin; TX
Spaceflight mechanics 1996 ; 1495-1504
ADVANCES IN THE ASTRONAUTICAL SCIENCES ; 93//pt2
1996-01-01
10 pages
Described as proceedings
Conference paper
English
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