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...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Hauptverfasser: Mazanek, D.D., Goodliff, K.E., Cornelius, D.M.
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 &amp; 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