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Author:

Kobzarenko, Igor

Title:

OPTIMAL DEFLECTION METHOD FOR A NEAR EARTH ASTEROID USING A LOW THRUST PROPULSION SYSTEM

Area of Honors:

Aerospace Engineering

Keywords:

Asteroid deflection
Low-Thrust
4179 Toutatis

File:

Download Kobzarenko_Igor_Thesis.pdf

Thesis Supervisors:

Robert Graham Melton, Thesis Supervisor
Cengiz Camci, Thesis Honors Advisor
David Bradley Spencer, Faculty Reader
Amy Ruth Pritchett, Faculty Reader