Technical Papers
Feb 11, 2012

LunarVader: Development and Testing of Lunar Drill in Vacuum Chamber and in Lunar Analog Site of Antarctica

Publication: Journal of Aerospace Engineering
Volume 26, Issue 1

Abstract

Future exploration of the Moon will require access to the subsurface and acquisition of samples for scientific analysis and ground truthing of water-ice and mineral reserves for in situ resource utilization purposes. The LunarVader drill described in this paper is a 1-m class drill and cuttings acquisition system enabling subsurface exploration of the Moon. The drill employs rotary-percussive action, which reduces the weight on bit and energy consumption. This drilling approach has been successfully used by previous lunar missions, such as the Soviet Luna 16, 20, and 24, and United States Apollo 15, 16, and 17. These missions and drilling systems are described in detail. The passive sample acquisition system of the LunarVader drill delivers cuttings directly into a sample cup or an instrument inlet port. The drill was tested in a vacuum chamber and penetrated various formations, such as a water-saturated lunar soil simulant (JSC-1A) at −80°C, water-ice, and rocks to a depth of 1 m. The system was also field tested in the lunar analog site on Ross Island, Antarctica, where it successfully penetrated to 1-m depth and acquired icy samples into a sample cup. During the chamber and field testing, the LunarVader demonstrated drilling at the 1-1-100-100 level; that is, it penetrated 1 m in approximately 1 h with roughly 100-W power and less than 100-N weight on bit. This corresponds to a total drilling energy of approximately 100 Whr. The drill system achieved high enough technology readiness to be considered as a viable option for future lunar missions, such as the South Pole-Aitken Basin Sample Return and Geophysical Network missions recently recommended by the Decadal Survey of the National Research Council, and commercial missions, such as Google Lunar X-Prize missions.

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Acknowledgments

The research reported in this paper was conducted by Honeybee Robotics under various contracts with the National Aeronautics and Space Administration, including Astrobiology Science and Technology for Exploring Planets and the Small Business Innovative Research program. Testing in Antarctica was supported by the United States Antarctic Program as part of the National Science Foundation Office of Polar Programs.

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Information & Authors

Information

Published In

Go to Journal of Aerospace Engineering
Journal of Aerospace Engineering
Volume 26Issue 1January 2013
Pages: 74 - 86

History

Received: Oct 1, 2011
Accepted: Feb 9, 2012
Published online: Feb 11, 2012
Published in print: Jan 1, 2013

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Authors

Affiliations

K. Zacny, M.ASCE [email protected]
Director, Exploration Technology, Honeybee Robotics, 398 W. Washington Blvd., Ste. 200, Pasadena, CA 91103 (corresponding author). E-mail: [email protected]
G. Paulsen
Systems Engineer, Honeybee Robotics, 398 W. Washington Blvd., Ste. 200, Pasadena, CA 91103.
M. Szczesiak
Mechanical Engineer, Honeybee Robotics, 398 W. Washington Blvd., Ste. 200, Pasadena, CA 91103.
J. Craft
Project Manager, Honeybee Robotics, 398 W. Washington Blvd., Ste. 200, Pasadena, CA 91103.
P. Chu
Senior Engineer, Honeybee Robotics, 1110 NASA Pkwy., Ste. 440, Houston, TX 77058.
C. McKay
Senior Scientist, NASA Ames Research Center, Building 35, Moffett Field, CA 94040.
B. Glass
Senior Scientist, NASA Ames Research Center, Building 35, Moffett Field, CA 94040.
A. Davila
Research Scientist, NASA Ames Research Center, Building 35, Moffett Field, CA 94040.
M. Marinova
Research Scientist, NASA Ames Research Center, Building 35, Moffett Field, CA 94040.
W. Pollard
Professor, Dept. of Geography, McGill Univ., Montreal, QB, Canada H3A 2K6.
W. Jackson
Professor, Texas Tech Univ., Lubbock, TX 79409.

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