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ISRU Pilot Excavator: Bucket Drum Scaling Experimental ResultsNASA’s Space Technology Mission Directorate (STMD) is funding the development of a robotic excavator called the “ISRU Pilot Excavator” (IPEx) which will be a technology demonstration of excavating and transporting 10 metric tons of lunar regolith on the surface of the moon with a 30kg-class robotic excavator. IPEx will be the next generation of robotic excavators to use bucket drums as excavation tools. This is an evolution of the Regolith Advanced Surface Systems Operations Robot (RASSOR) developed at NASA’s Kennedy Space Center (KSC).
Bucket drums are hollow cylinders with regularly spaced scoops around the perimeter. The drums rotate in one direction to collect regolith with the scoops. The regolith slides down an internal baffling system inside the drum which prevents the regolith from falling back out of the scoops (see Figure 1). The captured regolith can then be transported while held in the drum and then deposited by rotating the drum in the opposite direction allowing the regolith to slide back down the baffling and out of the excavation scoops. Bucket drums were developed by Lockheed Martin in 2008 and used on multiple robotic excavator prototypes ever since. However, the forces on a bucket drum and considerations for scaling have not been measured in detail. Bucket drums are challenging to model using classical blade\bucket equations because of their unique geometry. Therefore, this experiment was performed to measure the forces on three bucket drums of the same geometry at different scales. Small: 9.4” (239mm) dia. x 8.1” (206mm) width, Medium: 11.6” (294mm) dia. x 10” (254mm) width, and Large: 17” (432mm) dia. x 14.1” (358mm) width.
The test stand consisted of an actuated gantry with controlled motion in the vertical (Z) and horizontal (X) axes and a single rotation axis (R). The bucket drums were individually mounted to the rotary axis of the test stand and translated across a prepared bed of BP-1 lunar regolith simulant at a specified linear speed and cutting depth. The test stand was outfitted with a torque sensor in line with the rotation of the drum (R) and a 3 axis (X, Y, and Z) load cell. In addition to the three sizes of bucket drums the linear excavation speed and cutting depth were test variables.
The results of these experiments show the relationship between the three scales of bucket drums for factors such as: excavation force, torque due to regolith rotation inside the drum, excavation energy, time to fill, etc. and will be discussed in detail in this paper. This fundamental data will be used in the design of IPEx and can inform the design of future bucket drum excavators.
Document ID
20210025846
Acquisition Source
Kennedy Space Center
Document Type
Conference Paper
Authors
Jason Schuler
(Kennedy Space Center Merritt Island, Florida, United States)
Andrew Nick
(Kennedy Space Center Merritt Island, Florida, United States)
Kurt Leucht
(Kennedy Space Center Merritt Island, Florida, United States)
Austin Langton
(Kennedy Space Center Merritt Island, Florida, United States)
Drew Smith
(Kennedy Space Center Merritt Island, Florida, United States)
Date Acquired
December 13, 2021
Subject Category
Lunar And Planetary Science And Exploration
Meeting Information
Meeting: 18th Biennial International Conference of the ASCE - Earth and Space 2022
Location: Denver, CO
Country: US
Start Date: April 25, 2022
End Date: April 28, 2022
Sponsors: Colorado School of Mines, American Society of Civil Engineers
Funding Number(s)
WBS: 596118.04.65.76
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Technical Review
NASA Peer Committee
Keywords
RASSOR
Excavation
Bucket Drum
BP-1
ISRU Pilot Excavator
IPEx
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