Two programs, Hiltop I and Hiltop II, generate optimum trajectory data for electric propulsion missions of interest in exploration of solar system. Propulsion-system logic is activated by single program-input key; program modifications retain Hiltop I within framework of logic, so that Hiltop I input files, will run Hiltop II version and produce identical results as before.
Spacecraft trajectory
NASA Tech Briefs ; 4 , 4
1980-06-01
Miscellaneous
No indication
English
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