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A manned lunar outpost. Design considerations for three key elements in an initial manned lunar outpostThe Initial Manned Lunar Outpost (IMLO) is proposed as the initial permanent base for manned activities on the Moon. The study concentrated on identifying the equipment, support systems, and initial base configuration necessary to accomplish the various science, industrial and exploration activities planned. The primary concepts of the MLO were the use of hard modules for habitation areas creating a flexible, modular transportation system; designing a multi-functional vehicle; and using an overhead radiation protection system. The transportation system, dubbed the Lunar Mobile Surface Transport System (LMSTS), carries the hard modules to the surface of the moon and provides a method to move them to the desired location through the use of interchangeable pallets. The avionics pallets are changed-out with wheel and hitch pallets, transforming the LMSTS into a "tractor trailer" used with the Multi-Functional Vehicle (MFV). The modules are placed under the Regolith Support Structure (RSS) which provides a stable environment and radiation protection for the entire base. The overhead structure was chosen over simply burying the modules to provide a study on the advantages and disadvantages of this type of system. The advantages include easy access to the exterior of the modules, providing a protected area for vehicles and equipment used in EVA, and creating an area of constant temperature. Disadvantages include a need for prefabrication of structural components, including the preconstruction and construction phases of the initial MLO. The design approach taken considered existing and near-term materials and technology only, without the consideration of possible future building technologies.
Document ID
19890006603
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Bell, Larry
(Houston Univ. TX, United States)
Trotti, Guillermo
(Houston Univ. TX, United States)
Brown, Jeff
(Houston Univ. TX, United States)
Bhattacharya, Nilajan
(Houston Univ. TX, United States)
Moore, Nathan
(Houston Univ. TX, United States)
Polette, Tom
(Houston Univ. TX, United States)
Toups, Larry
(Houston Univ. TX, United States)
Date Acquired
September 5, 2013
Publication Date
June 13, 1988
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
NASA-CR-184632
NAS 1.26:184632
Report Number: NASA-CR-184632
Report Number: NAS 1.26:184632
Accession Number
89N15974
Funding Number(s)
CONTRACT_GRANT: NGT-21-002-080
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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