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Trajectories to Nab a NEA (Near-Earth Asteroid)In 2010 and 2011 NASA and KISS sponsored studies to investigate the feasibility of identifying, capturing, and returning an entire (albeit small) NEA to the vicinity of Earth, and concluded that a 40-kW solar electric propulsion system launched on an Atlas 551 provided sufficient propulsion to control an asteroid's trajectory. Once secured by the spacecraft, a NEA with a naturally close encounter with Earth is nudged over a few years to target a lunar gravity assist, capturing the object into Earth orbit. With further use of solar perturbations, up to 3,600,000 kg of NEA could be placed in high-lunar orbit.




Document ID
20150007871
Acquisition Source
Jet Propulsion Laboratory
Document Type
Conference Paper
External Source(s)
Authors
Landau, Damon
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Dankanich, John
(AeroDank, Inc. Cleveland, OH, United States)
Strange, Nathan
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Bellerose, Julie
(Carnegie-Mellon Univ. Moffett Field, CA, United States)
Llanos, Pedro
(GMV Aerospace and Defense S.A. Madrid, Spain)
Tantardini, Marco
(Planetary Society Pasadena, CA, United States)
Date Acquired
May 11, 2015
Publication Date
February 10, 2013
Subject Category
Lunar And Planetary Science And Exploration
Report/Patent Number
AAS 13-409
Report Number: AAS 13-409
Meeting Information
Meeting: AAS/AIAA Spaceflight Mechanics Meeting
Location: Kauai, HI
Country: United States
Start Date: February 10, 2013
End Date: February 14, 2013
Sponsors: American Astronautical Society, American Inst. of Aeronautics and Astronautics
Distribution Limits
Public
Copyright
Other
Keywords
solar electric propulsion
asteriod retrieval

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