Structural Definition and Mass Estimation of Lunar Surface Habitats for the Lunar Architecture Team Phase 2 (LAT-2) Study

The Lunar Architecture Team Phase 2 study defined and assessed architecture options for a Lunar Outpost at the Moon's South Pole. The Habitation Focus Element Team was responsible for developing concepts for all of the Habitats and pressurized logistics modules particular to each of the archite...

Full description

Bibliographic Details
Main Authors: Smith, Russell W., Wu, K, Chauncey, Dorsey, John T.
Format: Other/Unknown Material
Language:unknown
Published: 2008
Subjects:
Online Access:http://hdl.handle.net/2060/20080013395
id ftnasantrs:oai:casi.ntrs.nasa.gov:20080013395
record_format openpolar
spelling ftnasantrs:oai:casi.ntrs.nasa.gov:20080013395 2023-05-15T18:23:13+02:00 Structural Definition and Mass Estimation of Lunar Surface Habitats for the Lunar Architecture Team Phase 2 (LAT-2) Study Smith, Russell W. Wu, K, Chauncey Dorsey, John T. Unclassified, Unlimited, Publicly available March 03, 2008 application/pdf http://hdl.handle.net/2060/20080013395 unknown Document ID: 20080013395 http://hdl.handle.net/2060/20080013395 No Copyright CASI Lunar and Planetary Science and Exploration Earth and Space Conference 2008; 3-5 Mar. 2008; Long Beach, CA; United States 2008 ftnasantrs 2019-07-21T01:32:51Z The Lunar Architecture Team Phase 2 study defined and assessed architecture options for a Lunar Outpost at the Moon's South Pole. The Habitation Focus Element Team was responsible for developing concepts for all of the Habitats and pressurized logistics modules particular to each of the architectures, and defined the shapes, volumes and internal layouts considering human factors, surface operations and safety requirements, as well as Lander mass and volume constraints. The Structures Subsystem Team developed structural concepts, sizing estimates and mass estimates for the primary Habitat structure. In these studies, the primary structure was decomposed into a more detailed list of components to be sized to gain greater insight into concept mass contributors. Structural mass estimates were developed that captured the effect of major design parameters such as internal pressure load. Analytical and empirical equations were developed for each structural component identified. Over 20 different hard-shell, hybrid expandable and inflatable soft-shell Habitat and pressurized logistics module concepts were sized and compared to assess structural performance and efficiency during the study. Habitats were developed in three categories; Mini Habs that are removed from the Lander and placed on the Lunar surface, Monolithic habitats that remain on the Lander, and Habitats that are part of the Mobile Lander system. Each category of Habitat resulted in structural concepts with advantages and disadvantages. The same modular shell components could be used for the Mini Hab concept, maximizing commonality and minimizing development costs. Larger Habitats had higher volumetric mass efficiency and floor area than smaller Habitats (whose mass was dominated by fixed items such as domes and frames). Hybrid and pure expandable Habitat structures were very mass-efficient, but the structures technology is less mature, and the ability to efficiently package and deploy internal subsystems remains an open issue. Other/Unknown Material South pole NASA Technical Reports Server (NTRS) South Pole
institution Open Polar
collection NASA Technical Reports Server (NTRS)
op_collection_id ftnasantrs
language unknown
topic Lunar and Planetary Science and Exploration
spellingShingle Lunar and Planetary Science and Exploration
Smith, Russell W.
Wu, K, Chauncey
Dorsey, John T.
Structural Definition and Mass Estimation of Lunar Surface Habitats for the Lunar Architecture Team Phase 2 (LAT-2) Study
topic_facet Lunar and Planetary Science and Exploration
description The Lunar Architecture Team Phase 2 study defined and assessed architecture options for a Lunar Outpost at the Moon's South Pole. The Habitation Focus Element Team was responsible for developing concepts for all of the Habitats and pressurized logistics modules particular to each of the architectures, and defined the shapes, volumes and internal layouts considering human factors, surface operations and safety requirements, as well as Lander mass and volume constraints. The Structures Subsystem Team developed structural concepts, sizing estimates and mass estimates for the primary Habitat structure. In these studies, the primary structure was decomposed into a more detailed list of components to be sized to gain greater insight into concept mass contributors. Structural mass estimates were developed that captured the effect of major design parameters such as internal pressure load. Analytical and empirical equations were developed for each structural component identified. Over 20 different hard-shell, hybrid expandable and inflatable soft-shell Habitat and pressurized logistics module concepts were sized and compared to assess structural performance and efficiency during the study. Habitats were developed in three categories; Mini Habs that are removed from the Lander and placed on the Lunar surface, Monolithic habitats that remain on the Lander, and Habitats that are part of the Mobile Lander system. Each category of Habitat resulted in structural concepts with advantages and disadvantages. The same modular shell components could be used for the Mini Hab concept, maximizing commonality and minimizing development costs. Larger Habitats had higher volumetric mass efficiency and floor area than smaller Habitats (whose mass was dominated by fixed items such as domes and frames). Hybrid and pure expandable Habitat structures were very mass-efficient, but the structures technology is less mature, and the ability to efficiently package and deploy internal subsystems remains an open issue.
format Other/Unknown Material
author Smith, Russell W.
Wu, K, Chauncey
Dorsey, John T.
author_facet Smith, Russell W.
Wu, K, Chauncey
Dorsey, John T.
author_sort Smith, Russell W.
title Structural Definition and Mass Estimation of Lunar Surface Habitats for the Lunar Architecture Team Phase 2 (LAT-2) Study
title_short Structural Definition and Mass Estimation of Lunar Surface Habitats for the Lunar Architecture Team Phase 2 (LAT-2) Study
title_full Structural Definition and Mass Estimation of Lunar Surface Habitats for the Lunar Architecture Team Phase 2 (LAT-2) Study
title_fullStr Structural Definition and Mass Estimation of Lunar Surface Habitats for the Lunar Architecture Team Phase 2 (LAT-2) Study
title_full_unstemmed Structural Definition and Mass Estimation of Lunar Surface Habitats for the Lunar Architecture Team Phase 2 (LAT-2) Study
title_sort structural definition and mass estimation of lunar surface habitats for the lunar architecture team phase 2 (lat-2) study
publishDate 2008
url http://hdl.handle.net/2060/20080013395
op_coverage Unclassified, Unlimited, Publicly available
geographic South Pole
geographic_facet South Pole
genre South pole
genre_facet South pole
op_source CASI
op_relation Document ID: 20080013395
http://hdl.handle.net/2060/20080013395
op_rights No Copyright
_version_ 1766202770456576000