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Boom Retraction Mechanism as Part of Sample Acquisition System from Remote and Hazardous Extra-Terrestrial SitesThis paper discusses the development of a mechanism as part of a comet sampling system. The mechanism, known by the acronym BRAD for Boom Retraction and Deployment, is part of a mission proposal to return a comet regolith sample to earth. The mission proposal; CORSAIR for Comet Rendezvous, Sample Acquisition, Investigation, and Return, was coordinated by Johns Hopkins Applied Physics Lab in Laurel, MD as a response to the NASA 2017 New Frontiers AO or Announcement of Opportunity. BRAD functions as a means to tend and control a deployable boom that connects a sample projectile to the spacecraft.
Document ID
20190030898
Acquisition Source
Goddard Space Flight Center
Document Type
Conference Paper
Authors
Smith, Walter
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Nuth, Joseph
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Wegel, Donald
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Church, Joseph
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Barfknecht, Peter
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Date Acquired
September 20, 2019
Publication Date
September 18, 2019
Subject Category
Spacecraft Instrumentation And Astrionics
Report/Patent Number
GSFC-E-DAA-TN69939
Report Number: GSFC-E-DAA-TN69939
Meeting Information
Meeting: European Space Mechanisms and Tribology Symposium
Location: Munich
Country: Germany
Start Date: September 18, 2019
End Date: September 20, 2019
Sponsors: Orbital- und Hydrotechnologie Bremen System G.m.b.H., European Space Agency (ESA)
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Technical Review
Single Expert
Keywords
Comet Sample Acquisition Mechanism
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