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Mission Design Analysis for the Martian Moon Phobos: Close Flybys, Missed Thrusts, and Other In-Flight EntertainmentA robotic mission to the Martian moons Phobos and Deimos would offer a wealth of scientific information and serve as a useful precursor to potential human missions. In this paper, we investigate a prospective mission enabled by solar electric propulsion that would explore Phobos via a series of flybys followed by capture into orbit around the moon. Of particular interest are low-cost options for capture and walkdown to the target science orbits aided by multi-body effects due to the mutual gravitational interaction of Phobos and Mars. We also consider contingency operations in the event of missed thrust or maneuver execution errors.
Document ID
20170008228
Acquisition Source
Jet Propulsion Laboratory
Document Type
Conference Paper
External Source(s)
Authors
Stuart, Jeffrey
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
McElrath, Tim
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Petropoulos, Anastassios
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
September 1, 2017
Publication Date
August 9, 2015
Subject Category
Spacecraft Propulsion And Power
Lunar And Planetary Science And Exploration
Meeting Information
Meeting: AAS/AIAA Astrodynamics Specialist Conference 2015
Location: Vail, CO
Country: United States
Start Date: August 9, 2015
End Date: August 13, 2015
Sponsors: American Astronomical Society, American Inst. of Aeronautics and Astronautics
Distribution Limits
Public
Copyright
Other
Keywords
SEP
Mars
orbit determination

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