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An Overview of NASA's Asteroid Redirect Mission (ARM) ConceptThe National Aeronautics and Space Administration (NASA) is developing the Asteroid Redirect Mission (ARM) as a capability demonstration for future human exploration, including use of high-power solar electric propulsion, which allows for the efficient movement of large masses through deep space. The ARM will also demonstrate the capability to conduct proximity operations with natural space objects and crewed operations beyond the security of quick Earth return. The Asteroid Redirect Robotic Mission (ARRM), currently in formulation, will visit a large near-Earth asteroid (NEA), collect a multi-ton boulder from its surface, conduct a demonstration of a slow push planetary defense technique, and redirect the multi-ton boulder into a stable orbit around the Moon. Once returned to cislunar space in the mid-2020s, astronauts aboard an Orion spacecraft will dock with the robotic vehicle to explore the boulder and return samples to Earth. The ARM is part of NASA's plan to advance technologies, capabilities, and spaceflight experience needed for a human mission to the Martian system in the 2030s. The ARM and subsequent availability of the asteroidal material in cis-lunar space, provide significant opportunities to advance our knowledge of small bodies in the synergistic areas of science, planetary defense, and in-situ resource utilization (ISRU). NASA established the Formulation Assessment and Support Team (FAST), comprised of scientists, engineers, and technologists, which supported ARRM mission requirements formulation, answered specific questions concerning potential target asteroid physical properties, and produced a publically available report. The ARM Investigation Team is being organized to support ARM implementation and execution. NASA is also open to collaboration with its international partners and welcomes further discussions. An overview of the ARM robotic and crewed segments, including mission requirements, NEA targets, and mission operations, and a discussion of potential opportunities for participation with the ARM will be provided.
Document ID
20160008082
Acquisition Source
Johnson Space Center
Document Type
Abstract
Authors
Abell, P. A.
(NASA Johnson Space Center Houston, TX, United States)
Mazanek, D. D.
(NASA Langley Research Center Hampton, VA, United States)
Reeves, D. M.
(NASA Langley Research Center Hampton, VA, United States)
Chodas, P. W.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Gates, M. M.
(NASA Headquarters Washington, DC United States)
Johnson, L. N.
(NASA Headquarters Washington, DC United States)
Ticker, R. L.
(NASA Headquarters Washington, DC United States)
Date Acquired
June 29, 2016
Publication Date
July 2, 2016
Subject Category
Lunar And Planetary Science And Exploration
Space Transportation And Safety
Report/Patent Number
JSC-CN-36614
Report Number: JSC-CN-36614
Meeting Information
Meeting: Jupiter Trojan 2016: New Insights Early Solar System
Location: Sagamihara
Country: Japan
Start Date: July 2, 2016
End Date: July 4, 2016
Sponsors: Japan Aerospace Exploration Agency
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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