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Performance of Boeing LRV wheels in a lunar soil simulant. Report 1: Effect of wheel design and soilSix versions of the wire mesh wheel were laboratory tested in a lunar soil simulant, consisting of a crushed basalt with a grainsize distribution similar to that of samples collected during Apollo 11 and 12 flights, to determine their relative performance. The consistency of the soil was varied to cover a range of cohesive and frictional properties to simulate soil conditions assumed to exist on the moon. Programmed-slip and constant-slip tests conducted with the single wheel dynamometer system showed that the performance of the wheel covered with a metal chevron tread over 50 percent of its contact surface was slightly superior to that of other tread designs.
Document ID
19720021195
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Green, A. J.
(Army Engineer Waterways Experiment Station Vicksburg, MS, United States)
Melzer, K.
(Army Engineer Waterways Experiment Station Vicksburg, MS, United States)
Date Acquired
September 2, 2013
Publication Date
December 1, 1971
Subject Category
Space Sciences
Report/Patent Number
M-71-10
NASA-CR-127695
M-70-15
REPT-1
Report Number: M-71-10
Report Number: NASA-CR-127695
Report Number: M-70-15
Report Number: REPT-1
Accession Number
72N28845
Funding Number(s)
CONTRACT_GRANT: NASA ORDER H-68683-A
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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