A Method for Determining Approximate Propulsion Cutoff Conditions for Ballistic Interplanetary Trajectories

by Louis N. Rowell


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A method for determining approximate propulsion cutoff conditions for any ballistic-type inter- planetary trajectory. It is assumed that the heliocentric portion of the trajectory originates near perihelion of the heliocentric orbit. The necessary computation is made without using a large-scale digital computer, yet with sufficient accuracy for many planning and engineering design studies.

This report is part of the RAND Corporation Research memorandum series. The Research Memorandum was a product of the RAND Corporation from 1948 to 1973 that represented working papers meant to report current results of RAND research to appropriate audiences.

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