Problem of navigating rocket approaching planet from great distance, into circular orbit about planet with minimum fuel expenditure, is analyzed; effects of varying line of approach and radius of circular orbit. See also pt 1 indexed in Engineering Index 1953 p 94 from Mar 1953 issue.
Entry into circular orbits -- 2
Brit Interplanetary Soc -- J
British Interplanetary Society -- Journal ; 13 , n 1
1954
6 pages
Aufsatz (Zeitschrift)
Englisch
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