Designing Transfers to Geostationary Orbit Using Combined Chemical–Electric Propulsion
Author:
Affiliation:
1. Mechanical and Aerospace Engineering Department, University of Missouri–Columbia, Columbia, Missouri 65211
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.A33259
Reference19 articles.
1. StuhlingerE., Ion Propulsion for Space Flight, 1st ed., McGraw–Hill, New York, 1964, pp. 313–326.
2. Spacecraft Electric Propulsion-An Overview
3. Geosynchronous-Earth-Orbit Communication Satellite Deliveries with Integrated Electric Propulsion
4. SackettL. L.MalchowH. L.EdelbaumT. N. “Solar Electric Geocentric Transfer with Attitude Constraints: Analysis,” NASA CR-134927, Aug. 1975.
5. Highly efficient, very low-thrust transfer to geosynchronous orbit -Exact and approximate solutions
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