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Microspine Gripping Mechanism for Asteroid CaptureThis paper details the development and early testing of a compliant suspension for a microspine gripper device for asteroid capture or zero-gravity percussive drilling. The microspine gripper architecture is reviewed, and a proposed microspine suspension design is presented and discussed. Prototyping methods are discussed, as well as testing methods and results. A path forward is identified from the results of the testing completed thus far. Key findings include: the microspine concept has been established as a valid architecture and the compliant suspension exhibits the desired stiffness characteristics for good gripping behavior. These developments will aid in developing the capability to grasp irregularly shaped boulders in microgravity.
Document ID
20190003852
Acquisition Source
Jet Propulsion Laboratory
Document Type
Conference Paper
External Source(s)
Authors
Merriam, Ezekiel G.
(Brigham Young Univ. Provo, UT, United States)
Berg, Andrew B
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Willig, Andrew
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Parness, Aaron
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Frey, Tim
(Rochester Institute of Technology Rochester, NY, United States)
Howell, Larry L
(Brigham Young Univ. Provo, UT, United States)
Date Acquired
May 1, 2019
Publication Date
May 4, 2016
Subject Category
Lunar And Planetary Science And Exploration
Engineering (General)
Report/Patent Number
JPL-CL-16-0376
Report Number: JPL-CL-16-0376
Meeting Information
Meeting: Aerospace Mechanisms Symposium
Location: Santa Clara, CA
Country: United States
Start Date: May 4, 2016
End Date: May 6, 2016
Distribution Limits
Public
Copyright
Other

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