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
Link To Document :
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