Preliminary Design of Low-Thrust Interplanetary Missions

Flanagan, S.; Sims, J.

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NASA NTRS · 20210003001

Preliminary Design of Low-Thrust Interplanetary Missions

Flanagan, S.·Sims, J.

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Abstract

A direct optimization method intended to be used primarily for preliminary design of low-thrust interplanetary trajectories, including those with multiple gravity assists, is presented.

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Flanagan, S., Sims, J.. 1999-08-16. Preliminary Design of Low-Thrust Interplanetary Missions. https://ntrs.nasa.gov/citations/20210003001

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