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Concepts for Mars On-Orbit Robotic Sample Capture and TransferA potential Mars Sample Return (MSR) mission could require robotic autonomous capture and manipulation of an Orbital Sample (OS) before returning the samples to Earth. In one scenario, an orbiter would capture the OS, manipulate to a preferential orientation, transition it through the steps required to break-the-chain with Mars, stowing it in a containment vessel or an Earth Entry Vehicle (EEV) and providing redundant containment to the OS (for example by closing and sealing the lid of the EEV). In this paper, we discuss the trade-space of concepts generated for both the individual aspects of capture and manipulation of the OS, as well as concepts for the end-to-end system. Notably, we discuss concepts for OS capture, manipulation of the OS to orient it to a preferred configuration, and steps for transitioning the OS between different stages of manipulation, ultimately securing it in a containment vessel or Earth Entry Vehicle.



Document ID
20190028434
Acquisition Source
Jet Propulsion Laboratory
Document Type
Conference Paper
External Source(s)
Authors
Chamberlian-Simon, Brendan
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Mukherjee, Rudranarayan
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Smith, Russell
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Dolci, Marco
(Politecnico di Torino Torino, Italy)
Date Acquired
August 1, 2019
Publication Date
March 4, 2017
Subject Category
Space Transportation And Safety
Report/Patent Number
JPL-CL-CL#17-0368
Report Number: JPL-CL-CL#17-0368
Meeting Information
Meeting: IEEE Aerospace Conference
Location: Big Sky, MT
Country: United States
Start Date: March 4, 2017
End Date: March 11, 2017
Sponsors: Institute of Electrical and Electronics Engineers
Distribution Limits
Public
Copyright
Other

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