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Mars, Phobos, and Deimos Sample Return Enabled by ARRM Alternative Trade Study SpacecraftThe Asteroid Robotic Redirect Mission (ARRM) has been the topic of many mission design studies since 2011. The reference ARRM spacecraft uses a powerful solar electric propulsion (SEP) system and a bag device to capture a small asteroid from an Earth-like orbit and redirect it to a distant retrograde orbit (DRO) around the moon. The ARRM Option B spacecraft uses the same propulsion system and multi-Degree of Freedom (DoF) manipulators device to retrieve a very large sample (thousands of kilograms) from a 100+ meter diameter farther-away Near Earth Asteroid (NEA). This study will demonstrate that the ARRM Option B spacecraft design can also be used to return samples from Mars and its moons - either by acquiring a large rock from the surface of Phobos or Deimos, and or by rendezvousing with a sample-return spacecraft launched from the surface of Mars.
Document ID
20140017471
Acquisition Source
Goddard Space Flight Center
Document Type
Presentation
Authors
Englander, Jacob A.
(NASA Goddard Space Flight Center Greenbelt, MD United States)
Vavrina, Matthew
(AI Solutions, Inc. Lanham, MD, United States)
Merrill, Raymond G.
(NASA Langley Research Center Hampton, VA, United States)
Qu, Min
(Analytical Mechanics Associates, Inc. Hampton, VA, United States)
Naasz, Bo J.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Date Acquired
December 17, 2014
Publication Date
August 4, 2014
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
GSFC-E-DAA-TN16517
Meeting Information
Meeting: AIAA/AAS Astrodynamics Specialist Conference
Location: San Diego, CA
Country: United States
Start Date: August 4, 2014
End Date: August 7, 2014
Sponsors: American Inst. of Aeronautics and Astronautics, American Astronomical Society
Funding Number(s)
OTHER: 2014-595-ARRM
CONTRACT_GRANT: NNG14CR57C
CONTRACT_GRANT: NNL12AA09C
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
trajectory design
optimization
low thrust
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