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ID No : | 874 Edit | Title: | Comparison of ISRU Excavation System Model Blade Force Methodology and Experimental Results |
Summary / Review : | "An Excavation System Model has been written to simulate the collection and transportation of regolith on the Moon. The calculations in this model include an estimation of the forces on the digging tool as a result of excavation into the regolith. Verification testing has been performed and the forces recorded from this testing were compared to the calculated theoretical data. A prototype lunar vehicle built at the NASA Johnson Space Center (JSC) was tested with a bulldozer type blade developed at the NASA Kennedy Space Center (KSC) attached to the front. This is the initial correlation of actual field test data to the blade forces calculated by the Excavation System Model and the test data followed similar trends with the predicted values. This testing occurred in soils developed at the NASA Glenn Research Center (GRC) which are a mixture of different types of sands and whose soil properties have been well characterized. Three separate analytical models are compared to the test data." (Author's abstract) |
Author(s) : |
Gallo, Christopher A.; Wilkinson, R. Allen; Mueller, Robert P.; Schuler, Jason M.; Nick, Andrew J., [Glenn Research Center; Kennedy Space Center] |
Publication Date: | 2010 |
Category(s) : |
Bases, industry and manufacturing / Mining / Lunar |
Progress Type: | T ( A=Analysis only, D=Design, T=Testing, C=Completed or Commercial product ) |
Web URL : |
http://hdl.handle.net/2060/20100012787
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PERMANENT code(s) : | L,U |
(Explanation of the last 3 rows above) |
In the row above, there are up to 4 possibilities: U = URL you can click on to get a copy instantly from another source on the internet, or request it from that source D = Downloadable from PERMANENT (such as because no other URL known...) L = LAN copy, PERMANENT has a digital copy but not downloadable from our website P = Paper copy in the PERMANENT office Typically, only 0 to 3 methods are available. |
NTRS : | 20100012787 |
Other Ref # : | NASA/TM-2010-215591, E-16880 |
Submitted by : | MEP |
Comments: |
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