his chapter presents the vector-based approach to the classical problem of deter- ... 2.23 A hyperbolic earth departure trajectory has a perigee altitude of 300 km...692 pages. Associate Professor of Aerospace Engineering. COMMITTEE ... from the arrival hyperbolic trajectory and get onto a path staying in the Sun-planet system, or a.... by S Fritz Cited by 6 1Aerospace Engineering, San Jos State University, San Jos, CA 95192-0179, USA ... With , we have the time of arrival at and its positio
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