Maximizing Payload Mass Fractions of Spacecraft for Interplanetary Electric Propulsion Missions
Author:
Affiliation:
1. University of Michigan, University of Michigan
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.17433
Reference11 articles.
1. Preliminary Design of Nuclear Electric Propulsion Missions to the Outer Planets
2. Shape-Based Algorithm for the Automated Design of Low-Thrust, Gravity Assist Trajectories
3. Design of the First Interplanetary Solar Electric Propulsion Mission
4. Electric-propulsion spacecraft optimization for lunar missions
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