Solution to problem of transferring rocket between two terminals in space with minimum fuel expenditure; results obtained when application is made to number of particular problems of space navigation; mathematical techniques which may usefully be employed in calculation of optimum rocket trajectories, exemplified by method of obtaining maximum range from rocket missile over earth's surface. Bibliography.
Dynamic problems of interplanetary flight
Aeronautical Quarterly
Aeronautical Quarterly ; 6 , Part 3
1955
16 pages
Aufsatz (Zeitschrift)
Englisch
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