Descent Assisted Split Habitat Lunar Lander Concept
The descent assisted split habitat (DASH) lunar lander concept utilizes a disposable braking stage for descent and a minimally sized pressurized volume for crew transport to and from the lunar surface. The lander can also be configured to perform autonomous cargo missions. Although a braking-stage a...
Gespeichert in:
Hauptverfasser: | , , |
---|---|
Format: | Tagungsbericht |
Sprache: | eng |
Schlagworte: | |
Online-Zugang: | Volltext bestellen |
Tags: |
Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
|
container_end_page | 16 |
---|---|
container_issue | |
container_start_page | 1 |
container_title | |
container_volume | |
creator | Mazanek, D.D. Goodliff, K.E. Cornelius, D.M. |
description | The descent assisted split habitat (DASH) lunar lander concept utilizes a disposable braking stage for descent and a minimally sized pressurized volume for crew transport to and from the lunar surface. The lander can also be configured to perform autonomous cargo missions. Although a braking-stage approach represents a significantly different operational concept compared with a traditional two-stage lander, the DASH lander offers many important benefits. These benefits include improved crew egress/ingress and large-cargo unloading; excellent surface visibility during landing; elimination of the need for deep-throttling descent engines; potentially reduced plume-surface interactions and lower vertical touchdown velocity; and reduced lander gross mass through efficient mass staging and volume segmentation. This paper documents the conceptual study on various aspects of the design, including development of sortie and outpost lander configurations and a mission concept of operations; the initial descent trajectory design; the initial spacecraft sizing estimates and subsystem design; and the identification of technology needs. |
doi_str_mv | 10.1109/AERO.2008.4526498 |
format | Conference Proceeding |
fullrecord | <record><control><sourceid>proquest_6IE</sourceid><recordid>TN_cdi_ieee_primary_4526498</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><ieee_id>4526498</ieee_id><sourcerecordid>33561946</sourcerecordid><originalsourceid>FETCH-LOGICAL-i1648-a31d70cb00cedeed993d8938b61f0374c7a26c987f615159bce23b75cb9a9a3e3</originalsourceid><addsrcrecordid>eNpFkE1Lw0AYhNcvsK3-APGSk7fE3X338xhqtUKg4Ad4C5vNW1hJ05jdHPz3FlrwNId5ZhiGkDtGC8aofSxXb5uCU2oKIbkS1pyRORNcCCaMYedkxq1VOQdpLv4NDZdkdkjLHDh8XZN5jN-UcsoNnRF4wuixT1kZY4gJ2-x96ELK1q4JyaWsmno3ZpXrWxyz5b73OKQbcrV1XcTbky7I5_PqY7nOq83L67Ks8sCUMLkD1mrqG0o9toittdAaC6ZRbEtBC68dV94avVVMMmkbjxwaLX1jnXWAsCAPx95h3P9MGFO9C4exXed63E-xBpCKWaEO4P0RDIhYD2PYufG3Pl0Ef6P0VQo</addsrcrecordid><sourcetype>Aggregation Database</sourcetype><iscdi>true</iscdi><recordtype>conference_proceeding</recordtype><pqid>33561946</pqid></control><display><type>conference_proceeding</type><title>Descent Assisted Split Habitat Lunar Lander Concept</title><source>IEEE Electronic Library (IEL) Conference Proceedings</source><creator>Mazanek, D.D. ; Goodliff, K.E. ; Cornelius, D.M.</creator><creatorcontrib>Mazanek, D.D. ; Goodliff, K.E. ; Cornelius, D.M.</creatorcontrib><description>The descent assisted split habitat (DASH) lunar lander concept utilizes a disposable braking stage for descent and a minimally sized pressurized volume for crew transport to and from the lunar surface. The lander can also be configured to perform autonomous cargo missions. Although a braking-stage approach represents a significantly different operational concept compared with a traditional two-stage lander, the DASH lander offers many important benefits. These benefits include improved crew egress/ingress and large-cargo unloading; excellent surface visibility during landing; elimination of the need for deep-throttling descent engines; potentially reduced plume-surface interactions and lower vertical touchdown velocity; and reduced lander gross mass through efficient mass staging and volume segmentation. This paper documents the conceptual study on various aspects of the design, including development of sortie and outpost lander configurations and a mission concept of operations; the initial descent trajectory design; the initial spacecraft sizing estimates and subsystem design; and the identification of technology needs.</description><identifier>ISSN: 1095-323X</identifier><identifier>ISBN: 1424414873</identifier><identifier>ISBN: 9781424414871</identifier><identifier>EISSN: 2996-2358</identifier><identifier>EISBN: 1424414881</identifier><identifier>EISBN: 9781424414888</identifier><identifier>DOI: 10.1109/AERO.2008.4526498</identifier><language>eng</language><publisher>IEEE</publisher><subject>Biographies ; Engines ; Humans ; Moon ; NASA ; Payloads ; Propulsion ; Risk analysis ; Space technology ; Space vehicles</subject><ispartof>2008 IEEE Aerospace Conference, 2008, p.1-16</ispartof><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktohtml>$$Uhttps://ieeexplore.ieee.org/document/4526498$$EHTML$$P50$$Gieee$$H</linktohtml><link.rule.ids>309,310,780,784,789,790,2056,4047,4048,27923,54918</link.rule.ids><linktorsrc>$$Uhttps://ieeexplore.ieee.org/document/4526498$$EView_record_in_IEEE$$FView_record_in_$$GIEEE</linktorsrc></links><search><creatorcontrib>Mazanek, D.D.</creatorcontrib><creatorcontrib>Goodliff, K.E.</creatorcontrib><creatorcontrib>Cornelius, D.M.</creatorcontrib><title>Descent Assisted Split Habitat Lunar Lander Concept</title><title>2008 IEEE Aerospace Conference</title><addtitle>AERO</addtitle><description>The descent assisted split habitat (DASH) lunar lander concept utilizes a disposable braking stage for descent and a minimally sized pressurized volume for crew transport to and from the lunar surface. The lander can also be configured to perform autonomous cargo missions. Although a braking-stage approach represents a significantly different operational concept compared with a traditional two-stage lander, the DASH lander offers many important benefits. These benefits include improved crew egress/ingress and large-cargo unloading; excellent surface visibility during landing; elimination of the need for deep-throttling descent engines; potentially reduced plume-surface interactions and lower vertical touchdown velocity; and reduced lander gross mass through efficient mass staging and volume segmentation. This paper documents the conceptual study on various aspects of the design, including development of sortie and outpost lander configurations and a mission concept of operations; the initial descent trajectory design; the initial spacecraft sizing estimates and subsystem design; and the identification of technology needs.</description><subject>Biographies</subject><subject>Engines</subject><subject>Humans</subject><subject>Moon</subject><subject>NASA</subject><subject>Payloads</subject><subject>Propulsion</subject><subject>Risk analysis</subject><subject>Space technology</subject><subject>Space vehicles</subject><issn>1095-323X</issn><issn>2996-2358</issn><isbn>1424414873</isbn><isbn>9781424414871</isbn><isbn>1424414881</isbn><isbn>9781424414888</isbn><fulltext>true</fulltext><rsrctype>conference_proceeding</rsrctype><creationdate>2008</creationdate><recordtype>conference_proceeding</recordtype><sourceid>6IE</sourceid><sourceid>RIE</sourceid><recordid>eNpFkE1Lw0AYhNcvsK3-APGSk7fE3X338xhqtUKg4Ad4C5vNW1hJ05jdHPz3FlrwNId5ZhiGkDtGC8aofSxXb5uCU2oKIbkS1pyRORNcCCaMYedkxq1VOQdpLv4NDZdkdkjLHDh8XZN5jN-UcsoNnRF4wuixT1kZY4gJ2-x96ELK1q4JyaWsmno3ZpXrWxyz5b73OKQbcrV1XcTbky7I5_PqY7nOq83L67Ks8sCUMLkD1mrqG0o9toittdAaC6ZRbEtBC68dV94avVVMMmkbjxwaLX1jnXWAsCAPx95h3P9MGFO9C4exXed63E-xBpCKWaEO4P0RDIhYD2PYufG3Pl0Ef6P0VQo</recordid><startdate>2008</startdate><enddate>2008</enddate><creator>Mazanek, D.D.</creator><creator>Goodliff, K.E.</creator><creator>Cornelius, D.M.</creator><general>IEEE</general><scope>6IE</scope><scope>6IH</scope><scope>CBEJK</scope><scope>RIE</scope><scope>RIO</scope><scope>7SP</scope><scope>8FD</scope><scope>H8D</scope><scope>L7M</scope></search><sort><creationdate>2008</creationdate><title>Descent Assisted Split Habitat Lunar Lander Concept</title><author>Mazanek, D.D. ; Goodliff, K.E. ; Cornelius, D.M.</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-i1648-a31d70cb00cedeed993d8938b61f0374c7a26c987f615159bce23b75cb9a9a3e3</frbrgroupid><rsrctype>conference_proceedings</rsrctype><prefilter>conference_proceedings</prefilter><language>eng</language><creationdate>2008</creationdate><topic>Biographies</topic><topic>Engines</topic><topic>Humans</topic><topic>Moon</topic><topic>NASA</topic><topic>Payloads</topic><topic>Propulsion</topic><topic>Risk analysis</topic><topic>Space technology</topic><topic>Space vehicles</topic><toplevel>online_resources</toplevel><creatorcontrib>Mazanek, D.D.</creatorcontrib><creatorcontrib>Goodliff, K.E.</creatorcontrib><creatorcontrib>Cornelius, D.M.</creatorcontrib><collection>IEEE Electronic Library (IEL) Conference Proceedings</collection><collection>IEEE Proceedings Order Plan (POP) 1998-present by volume</collection><collection>IEEE Xplore All Conference Proceedings</collection><collection>IEEE Electronic Library (IEL)</collection><collection>IEEE Proceedings Order Plans (POP) 1998-present</collection><collection>Electronics & Communications Abstracts</collection><collection>Technology Research Database</collection><collection>Aerospace Database</collection><collection>Advanced Technologies Database with Aerospace</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>Mazanek, D.D.</au><au>Goodliff, K.E.</au><au>Cornelius, D.M.</au><format>book</format><genre>proceeding</genre><ristype>CONF</ristype><atitle>Descent Assisted Split Habitat Lunar Lander Concept</atitle><btitle>2008 IEEE Aerospace Conference</btitle><stitle>AERO</stitle><date>2008</date><risdate>2008</risdate><spage>1</spage><epage>16</epage><pages>1-16</pages><issn>1095-323X</issn><eissn>2996-2358</eissn><isbn>1424414873</isbn><isbn>9781424414871</isbn><eisbn>1424414881</eisbn><eisbn>9781424414888</eisbn><abstract>The descent assisted split habitat (DASH) lunar lander concept utilizes a disposable braking stage for descent and a minimally sized pressurized volume for crew transport to and from the lunar surface. The lander can also be configured to perform autonomous cargo missions. Although a braking-stage approach represents a significantly different operational concept compared with a traditional two-stage lander, the DASH lander offers many important benefits. These benefits include improved crew egress/ingress and large-cargo unloading; excellent surface visibility during landing; elimination of the need for deep-throttling descent engines; potentially reduced plume-surface interactions and lower vertical touchdown velocity; and reduced lander gross mass through efficient mass staging and volume segmentation. This paper documents the conceptual study on various aspects of the design, including development of sortie and outpost lander configurations and a mission concept of operations; the initial descent trajectory design; the initial spacecraft sizing estimates and subsystem design; and the identification of technology needs.</abstract><pub>IEEE</pub><doi>10.1109/AERO.2008.4526498</doi><tpages>16</tpages><oa>free_for_read</oa></addata></record> |
fulltext | fulltext_linktorsrc |
identifier | ISSN: 1095-323X |
ispartof | 2008 IEEE Aerospace Conference, 2008, p.1-16 |
issn | 1095-323X 2996-2358 |
language | eng |
recordid | cdi_ieee_primary_4526498 |
source | IEEE Electronic Library (IEL) Conference Proceedings |
subjects | Biographies Engines Humans Moon NASA Payloads Propulsion Risk analysis Space technology Space vehicles |
title | Descent Assisted Split Habitat Lunar Lander Concept |
url | https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-14T06%3A17%3A30IST&url_ver=Z39.88-2004&url_ctx_fmt=infofi/fmt:kev:mtx:ctx&rfr_id=info:sid/primo.exlibrisgroup.com:primo3-Article-proquest_6IE&rft_val_fmt=info:ofi/fmt:kev:mtx:book&rft.genre=proceeding&rft.atitle=Descent%20Assisted%20Split%20Habitat%20Lunar%20Lander%20Concept&rft.btitle=2008%20IEEE%20Aerospace%20Conference&rft.au=Mazanek,%20D.D.&rft.date=2008&rft.spage=1&rft.epage=16&rft.pages=1-16&rft.issn=1095-323X&rft.eissn=2996-2358&rft.isbn=1424414873&rft.isbn_list=9781424414871&rft_id=info:doi/10.1109/AERO.2008.4526498&rft_dat=%3Cproquest_6IE%3E33561946%3C/proquest_6IE%3E%3Curl%3E%3C/url%3E&rft.eisbn=1424414881&rft.eisbn_list=9781424414888&disable_directlink=true&sfx.directlink=off&sfx.report_link=0&rft_id=info:oai/&rft_pqid=33561946&rft_id=info:pmid/&rft_ieee_id=4526498&rfr_iscdi=true |