Design Development Strategy for the Mars Surface Astrobiology Laboratory

Cohen, Marc M.

doi:10.4271/2000-01-2344

Cited by 3 publications

(4 citation statements)

References 18 publications

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“…Of necessity, in-space laboratories depart from the leading trend in contemporary terrestrial laboratory design practice: "open plan" configurations. 5 The harsh economics of space architecture force contained-module, closed-plan laboratories until extensive in situ construction can be achieved. This means the ISS precedent and other volumeconstrained mobile laboratories are appropriate starting points for adaptation based on planet-surface conditions and the expanded laboratory functional programs described above.…”

Section: Laboratory Module Architecture Optionsmentioning

confidence: 99%

Module Architecture for In Situ Space Laboratories

Sherwood

2010

40th International Conference on Environmental Systems

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The paper analyzes internal outfitting architectures for space exploration laboratory modules. ISS laboratory architecture is examined as a baseline for comparison; applicable insights are derived. Laboratory functional programs are defined for seven planet-surface knowledge domains. Necessary and value-added departures from the ISS architecture standard are defined, and three sectional interior architecture options are assessed for practicality and potential performance. Contemporary guidelines for terrestrial analytical laboratory design are found to be applicable to the in-space functional program. Densepacked racks of system equipment, and high module volume packing ratios, should not be assumed as the default solution for exploration laboratories whose primary activities include un-scriptable investigations and experimentation on the system equipment itself.

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Section: Laboratory Module Architecture Optionsmentioning

confidence: 99%

Module Architecture for In Situ Space Laboratories

Sherwood

2010

40th International Conference on Environmental Systems

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“…Two of the surveyed rover concepts included a sample airlock: Griffin (1990) andESA (2000). In combination with an astrobiology "glovebox" research chamber (Cohen, 2000), it holds the key to examining scientific samples inside the pressurized rover while an EVA team of two or more crew members is exploring the terrain on foot outside the rover. The crewmembers collect rocks, soil, and other materials, and place it in a protective containment.…”

Section: Scientific Sample Airlocksmentioning

confidence: 99%

“…Instead, it becomes necessary only to pump down or bleed off a very small interstitial volume between the space suit backpack and the "airlockless" inner hatch. The precedents for this strategy include the "Suitport" idea, the NASA-Ames Hazmat vehicle shown in FIGURE 5, and the HamiltonSundstrand "Ready to Wear" Marssuit (Hodgeson & Guyer, 1998, 2000.…”

Section: Triple Volume Strategymentioning

confidence: 99%

“…The sample airlock consists of a (usually) cylindrical shell that spans two working environments: the exterior ambient environment of the moon or planet and the working environment inside a research chamber glovebox (Cohen, 1999(Cohen, & 2000. The main mechanical parts are the inner and outer hatches, that require a high degree of reliability to ensure proper opening, closing, latching and sealing.…”

Section: Features Of the Scientific Sample Airlockmentioning

confidence: 99%

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Pressurized Rover Airlocks

Cohen¹

2000

SAE Technical Paper Series

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The ability for crewmembers to explore the surface of the Moon or Mars effectively on foot remains a significant test of any exploration design.The availability of a pressurized rover would substantially increase the range of exploration by space suited crewmembers. The design of the airlock systems or functions will facilitate crewmembers in accomplishing these efforts. The pressurized rover for planetary exploration incorporates three types of airlocks or pressure ports: the EVA airlock, the sample airlock and the habitat docking port. This paper conducts a survey of selected precedents in pressurized rover design and then analyzes the key issues for airlock design.

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Building the Test Bed SHEE- A Self Deployable Habitat for Extreme Environments Lessons Learnt and Exploitation Opportunities for the Scientific Community

Imhof

Hoheneder

Ransom

et al. 2015

AIAA SPACE 2015 Conference and Exposition

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This paper presents preliminary results of the qualification and testing campaign for the Self Deployable Habitat for Extreme Environments (SHEE). Developed under a three yearEuropean Commission FP7 grant, the SHEE is a rigid segment deployable habitat test bed designed for use in space analogous environments. The objective of the SHEE project is to develop a self-deployable habitat test bed that will support a crew of two for a period of up to two weeks in duration. During this time the habitat will provide for all of the environmental, hygiene, dietary, logistical, professional, and psychological needs of the crew. Unlike most space analog habitats, the SHEE will use commercial transportation infrastructure, allowing for cost effective transportation to space analog sites across Europe. Once on site, the habitat will be autonomously deployed with no human intervention required, and will be able to re-pack itself with minimal human assistance. Qualification and testing of the fully outfitted SHEE test-bed began in April of 2015 at COMEX in Marseille, and will conclude in October of 2015 at the International Space University in Strasbourg. The testing campaign has included a shake-down of all subsystems, thermal analysis, stress analysis, a habitability study, acoustic tests and more. At the conclusion of the project in December of 2015, the SHEE will be made available to the European scientific community for analog space simulations. The first field deployment of the SHEE will occur in 2016 as part of the Moonwalk FP7 campaign in Rio Tinto, Spain. It is anticipated that elements of the SHEE design will find practical applications in any hostile environment requiring an extended human presence, on or off the Earth.Downloaded by UNIVERSITY OF GLASGOW on October 12, 2015 | http://arc.aiaa.org |

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Design Development Strategy for the Mars Surface Astrobiology Laboratory

Cited by 3 publications

References 18 publications

Module Architecture for In Situ Space Laboratories

Module Architecture for In Situ Space Laboratories

Pressurized Rover Airlocks

Building the Test Bed SHEE- A Self Deployable Habitat for Extreme Environments Lessons Learnt and Exploitation Opportunities for the Scientific Community

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