NASA Oxygen and Water Production Architectures for Early Reusable Lander
The presentation covers two recent studies Lunar In Situ Resource Utilization (ISRU) systems to produce propellant for an early reusable lander architecture. The first study examines the hardware, power, and operations required to produce 10 metric tons of oxygen per year near the lunar south pole u...
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ftnasantrs:oai:casi.ntrs.nasa.gov:20190028813 2023-05-15T18:22:03+02:00 NASA Oxygen and Water Production Architectures for Early Reusable Lander Paz, Aaron J. Moore, Landon A. Kleinhenz, Julie E. Linne, D. Sanders, G. Unclassified, Unlimited, Publicly available July 17, 2019 application/pdf http://hdl.handle.net/2060/20190028813 unknown Document ID: 20190028813 http://hdl.handle.net/2060/20190028813 Copyright, Public use permitted CASI Life Sciences (General) JSC-E-DAA-TN70609 Lunar In Situ Resource Utilization (ISRU) Workshop; Jul 15, 2019 - Jul 17, 2019; Columbia, MD; United States 2019 ftnasantrs 2019-08-31T23:12:19Z The presentation covers two recent studies Lunar In Situ Resource Utilization (ISRU) systems to produce propellant for an early reusable lander architecture. The first study examines the hardware, power, and operations required to produce 10 metric tons of oxygen per year near the lunar south pole using the Carbothermal Reduction process. The second study examines the hardware, power, and operations to mine and process 15 metric tons of water from a permanently shadowed crater near Shackleton crater. Other/Unknown Material South pole NASA Technical Reports Server (NTRS) Shackleton South Pole |
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Open Polar |
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NASA Technical Reports Server (NTRS) |
op_collection_id |
ftnasantrs |
language |
unknown |
topic |
Life Sciences (General) |
spellingShingle |
Life Sciences (General) Paz, Aaron J. Moore, Landon A. Kleinhenz, Julie E. Linne, D. Sanders, G. NASA Oxygen and Water Production Architectures for Early Reusable Lander |
topic_facet |
Life Sciences (General) |
description |
The presentation covers two recent studies Lunar In Situ Resource Utilization (ISRU) systems to produce propellant for an early reusable lander architecture. The first study examines the hardware, power, and operations required to produce 10 metric tons of oxygen per year near the lunar south pole using the Carbothermal Reduction process. The second study examines the hardware, power, and operations to mine and process 15 metric tons of water from a permanently shadowed crater near Shackleton crater. |
format |
Other/Unknown Material |
author |
Paz, Aaron J. Moore, Landon A. Kleinhenz, Julie E. Linne, D. Sanders, G. |
author_facet |
Paz, Aaron J. Moore, Landon A. Kleinhenz, Julie E. Linne, D. Sanders, G. |
author_sort |
Paz, Aaron J. |
title |
NASA Oxygen and Water Production Architectures for Early Reusable Lander |
title_short |
NASA Oxygen and Water Production Architectures for Early Reusable Lander |
title_full |
NASA Oxygen and Water Production Architectures for Early Reusable Lander |
title_fullStr |
NASA Oxygen and Water Production Architectures for Early Reusable Lander |
title_full_unstemmed |
NASA Oxygen and Water Production Architectures for Early Reusable Lander |
title_sort |
nasa oxygen and water production architectures for early reusable lander |
publishDate |
2019 |
url |
http://hdl.handle.net/2060/20190028813 |
op_coverage |
Unclassified, Unlimited, Publicly available |
geographic |
Shackleton South Pole |
geographic_facet |
Shackleton South Pole |
genre |
South pole |
genre_facet |
South pole |
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CASI |
op_relation |
Document ID: 20190028813 http://hdl.handle.net/2060/20190028813 |
op_rights |
Copyright, Public use permitted |
_version_ |
1766201396428800000 |