DocumentCode
1938120
Title
Sample Acquisition and Caching architecture for the Mars Sample Return mission
Author
Zacny, K. ; Chu, Peter ; Cohen, Johanne ; Paulsen, Gard ; Craft, J. ; Szwarc, T.
Author_Institution
Honeybee Robot., Pasadena, CA, USA
fYear
2013
fDate
2-9 March 2013
Firstpage
1
Lastpage
12
Abstract
This paper presents a Mars Sample Return (MSR) Sample Acquisition and Caching (SAC) study developed for the three rover platforms: MER, MER+, and MSL. The study took into account 26 SAC requirements provided by the NASA Mars Exploration Program Office. For this SAC architecture, the reduction of mission risk was chosen by us as having greater priority than mass or volume. For this reason, we selected a “One Bit per Core” approach. The enabling technology for this architecture is Honeybee Robotics´ “eccentric tubes” core breakoff approach. The breakoff approach allows the drill bits to be relatively small in diameter and in turn lightweight. Hence, the bits could be returned to Earth with the cores inside them with only a modest increase to the total returned mass, but a significant decrease in complexity. Having dedicated bits allows a reduction in the number of core transfer steps and actuators. It also alleviates the bit life problem, eliminates cross contamination, and aids in hermetic sealing. An added advantage is faster drilling time, lower power, lower energy, and lower Weight on Bit (which reduces Arm preload requirements). Drill bits are based on the BigTooth bit concept, which allows re-use of the same bit multiple times, if necessary. The proposed SAC consists of a 1) Rotary-Percussive Core Drill, 2) Bit Storage Carousel, 3) Cache, 4) Robotic Arm, and 5) Rock Abrasion and Brushing Bit (RABBit), which is deployed using the Drill. The system also includes PreView bits (for viewing of cores prior to caching) and Powder bits for acquisition of regolith or cuttings. The SAC total system mass is less than 22 kg for MER and MER+ size rovers and less than 32 kg for the MSL-size rover.
Keywords
Earth; Mars; aerospace control; space vehicles; Earth; MER; MSL; Mars sample return mission; NASA Mars exploration program office; PreView bits; RABBit; SAC architecture; SAC requirements; actuators; bit storage carousel; brushing bit; cache; caching architecture; core transfer steps; cross contamination; hermetic sealing; honeybee robotics eccentric tube core breakoff approach; mission risk reduction; robotic arm; rock abrasion; rotary-percussive core drill; sample acquisition; Brushes; Electron tubes; Mars; Powders; Rabbits; Robots; Rocks;
fLanguage
English
Publisher
ieee
Conference_Titel
Aerospace Conference, 2013 IEEE
Conference_Location
Big Sky, MT
ISSN
1095-323X
Print_ISBN
978-1-4673-1812-9
Type
conf
DOI
10.1109/AERO.2013.6497187
Filename
6497187
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