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Soil Transport ImplementThe design of the Soil Transport Implement (STI) for SKITTER is presented. The purpose of STI is to provide a protective layer of lunar soil for the lunar modules. The objective is to cover the lunar module with a layer of soil approximately two meters thick within a two week period. The amount of soil required to cover the module is roughly 77 dump truck loads or three million earth pounds. A spinning disk is employed to accomplish its task. STI is an autonomous, teleoperated system. The design incorporates the latest advances in composite materials and high strength, light weight alloys to achieve a high strength to weight ratio. The preliminary design should only be used to assess the feasibility of employing a spinning wheel as a soil transport implement. A mathematical model of the spinning wheel was used to evaluate the performance of this design.
Document ID
19900014266
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Dixon, William
(Georgia Inst. of Tech. Atlanta, GA, United States)
Fan, William
(Georgia Inst. of Tech. Atlanta, GA, United States)
Lloyd, Joey
(Georgia Inst. of Tech. Atlanta, GA, United States)
Pham, Nam-Anh
(Georgia Inst. of Tech. Atlanta, GA, United States)
Stevens, Michael
(Georgia Inst. of Tech. Atlanta, GA, United States)
Date Acquired
September 6, 2013
Publication Date
March 1, 1988
Subject Category
Engineering (General)
Report/Patent Number
NASA-CR-184931
ME-4182
NAS 1.26:184931
Report Number: NASA-CR-184931
Report Number: ME-4182
Report Number: NAS 1.26:184931
Accession Number
90N23582
Funding Number(s)
CONTRACT_GRANT: NGT-21-002-800
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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