If rocket fails to follow previously computed trajectory in space, it will become necessary to correct its erroneous orbit by small thrusts from motors; it is proved that, if instant at which correction is to be made has been chosen, appropriate velocity increment to be given to rocket is uniquely determined; scheme for assisting navigator by calculating numerical tables prior to rocket's departure.
Correction of interplanetary orbits
Brit Interplanetary Soc -- J
British Interplanetary Society -- Journal ; 13 , n 4
1954
9 pages
Aufsatz (Zeitschrift)
Englisch
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