A payload-centric approach towards resilient and robust electric-propulsion enabled constellation mission design

A payload-centric approach towards resilient and robust electric-propulsion enabled constellation mission design

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Thesis: S.M., Massachusetts Institute of Technology, Department of Aeronautics and Astronautics, 2017.

Bibliographic Details
Main Author: Graham, John Kyle
Other Authors: Olivier de Weck and Afreen Siddiqi.
Format: Thesis
Language:eng
Published: Massachusetts Institute of Technology 2017
Subjects:
Aeronautics and Astronautics.
Online Access:http://hdl.handle.net/1721.1/112463

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