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NASA's Asteroid Redirect Mission: The Boulder Capture OptionNASA is examining two options for the Asteroid Redirect Mission (ARM), which will return asteroid material to a Lunar Distant Retrograde Orbit (LDRO) using a robotic solar-electric-propulsion spacecraft, called the Asteroid Redirect Vehicle (ARV). Once the ARV places the asteroid material into the LDRO, a piloted mission will rendezvous and dock with the ARV. After docking, astronauts will conduct two extravehicular activities (EVAs) to inspect and sample the asteroid material before returning to Earth. One option involves capturing an entire small (approximately 4-10 m diameter) near-Earth asteroid (NEA) inside a large inflatable bag. However, NASA is examining another option that entails retrieving a boulder (approximately 1-5 m) via robotic manipulators from the surface of a larger (approximately 100+ m) pre-characterized NEA. This option can leverage robotic mission data to help ensure success by targeting previously (or soon to be) well-characterized NEAs. For example, the data from the Hayabusa mission has been utilized to develop detailed mission designs that assess options and risks associated with proximity and surface operations. Hayabusa's target NEA, Itokawa, has been identified as a valid target and is known to possess hundreds of appropriately sized boulders on its surface. Further robotic characterization of additional NEAs (e.g., Bennu and 1999 JU3) by NASA's OSIRIS REx and JAXA's Hayabusa 2 missions is planned to begin in 2018. The boulder option is an extremely large sample‐return mission with the prospect of bringing back many tons of well‐characterized asteroid material to the Earth‐Moon system. The candidate boulder from the target NEA can be selected based on inputs from the world‐wide science community, ensuring that the most scientifically interesting boulder be returned for subsequent sampling. This boulder option for NASA's ARM can leverage knowledge of previously characterized NEAs from prior robotic missions, which provides more certainty of the target NEA's physical characteristics and reduces mission risk. This increases the return on investment for NASA's future activities with respect to science, human exploration, resource utilization, and planetary defense
Document ID
20140013143
Acquisition Source
Johnson Space Center
Document Type
Conference Paper
Authors
Abell, Paul A.
(NASA Johnson Space Center Houston, TX, United States)
Nuth, J.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Mazanek, D.
(NASA Langley Research Center Hampton, VA, United States)
Merrill, R.
(NASA Langley Research Center Hampton, VA, United States)
Reeves, D.
(NASA Langley Research Center Hampton, VA, United States)
Naasz, B.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Date Acquired
October 22, 2014
Publication Date
November 9, 2014
Subject Category
Lunar And Planetary Science And Exploration
Report/Patent Number
JSC-CN-32111
Meeting Information
Meeting: Annual Meeting of the Division for Planetary Sciences
Location: Tuscon, AZ
Country: United States
Start Date: November 9, 2014
End Date: November 14, 2014
Sponsors: American Astronomical Society
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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