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NASA NTRS · 20160001873

Global Optimization of Low-Thrust Interplanetary Trajectories Subject to Operational Constraints

Englander, Jacob Aldo·Vavrina, Matthew·Hinckley, David
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Abstract

Low-thrust electric propulsion provides many advantages for mission to difficult targets-Comets and asteroids-Mercury-Outer planets (with sufficient power supply)Low-thrust electric propulsion is characterized by high power requirements but also very high specific impulse (Isp), leading to very good mass fractions. Low-thrust trajectory design is a very different process from chemical trajectory.

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Englander, Jacob Aldo, Vavrina, Matthew, Hinckley, David. 2016-02-16. Global Optimization of Low-Thrust Interplanetary Trajectories Subject to Operational Constraints. https://ntrs.nasa.gov/citations/20160001873

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