Update on Subsonic Single Aft Engine (SUSAN) Electrofan Trade Space Exploration
NASA is conducting an ongoing trade study analysis of the SUSAN Electrofan aircraft concept, which utilizes 20-MW-class electrified aircraft propulsion to enable propulsive, aerodynamic, and control benefits while retaining the range, speed, and size of typical narrow-body regional aircraft. The stu...
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 | |
---|---|
container_issue | |
container_start_page | |
container_title | |
container_volume | |
creator | Jansen, Ralph H Kiris, Cetin C Chau, Timothy Machado, Leonardo Dever, Timothy P Litt, Jonathan S Arthur, Jarvis J Lynde, Michelle N Chapman, Jeffryes W Kratz, Jonathan L Turner, Mark G Mirhashemi, Arman Denham, Casey L Wishart, Jacob M Mahavier, Kendall Boucher, Matthew J Heersema, Nic Stalcup, Erik J |
description | NASA is conducting an ongoing trade study analysis of the SUSAN Electrofan aircraft concept, which utilizes 20-MW-class electrified aircraft propulsion to enable propulsive, aerodynamic, and control benefits while retaining the range, speed, and size of typical narrow-body regional aircraft. The study is constrained by the ground rules of operating within the current airport and airspace infrastructure. This ongoing study seeks to find a configuration and combination of technologies that yield significant fuel burn and emissions benefits. Another key goal is to reduce cost per passenger mile. Currently, the study is focused on a configuration that utilizes jet A or sustainable aviation fuels, however, we plan to consider other fuel alternatives in the future. This paper describes the progress in defining the architecture of the aircraft, engine, power system, control system, and initial understandings of the sensitivity of the potential configurations to technology assumptions based on key performance parameters. Additionally, progress towards definition and refinement of driving operational, economic, infrastructure, certification, and technical requirements is discussed. |
format | Conference Proceeding |
fullrecord | <record><control><sourceid>nasa_CYI</sourceid><recordid>TN_cdi_nasa_ntrs_20220011269</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>20220011269</sourcerecordid><originalsourceid>FETCH-nasa_ntrs_202200112693</originalsourceid><addsrcrecordid>eNqFybEKwjAQANAsDqL-gcONOghphELHUiJOOqSdy5leSiBcQhLBz3dxd3rD24rnlBasBJHBvF8lsrdgPK-BoHcVNK-eCU5mMv3jDDqQrTk6ZBgzLgQmoSXQnxRixuoj78XGYSh0-LkTx5seh_uFseDMNZdZSaWkbBrVdtc__QU0uDD-</addsrcrecordid><sourcetype>Publisher</sourcetype><iscdi>true</iscdi><recordtype>conference_proceeding</recordtype></control><display><type>conference_proceeding</type><title>Update on Subsonic Single Aft Engine (SUSAN) Electrofan Trade Space Exploration</title><source>NASA Technical Reports Server</source><creator>Jansen, Ralph H ; Kiris, Cetin C ; Chau, Timothy ; Machado, Leonardo ; Dever, Timothy P ; Litt, Jonathan S ; Arthur, Jarvis J ; Lynde, Michelle N ; Chapman, Jeffryes W ; Kratz, Jonathan L ; Turner, Mark G ; Mirhashemi, Arman ; Denham, Casey L ; Wishart, Jacob M ; Mahavier, Kendall ; Boucher, Matthew J ; Heersema, Nic ; Stalcup, Erik J</creator><creatorcontrib>Jansen, Ralph H ; Kiris, Cetin C ; Chau, Timothy ; Machado, Leonardo ; Dever, Timothy P ; Litt, Jonathan S ; Arthur, Jarvis J ; Lynde, Michelle N ; Chapman, Jeffryes W ; Kratz, Jonathan L ; Turner, Mark G ; Mirhashemi, Arman ; Denham, Casey L ; Wishart, Jacob M ; Mahavier, Kendall ; Boucher, Matthew J ; Heersema, Nic ; Stalcup, Erik J</creatorcontrib><description>NASA is conducting an ongoing trade study analysis of the SUSAN Electrofan aircraft concept, which utilizes 20-MW-class electrified aircraft propulsion to enable propulsive, aerodynamic, and control benefits while retaining the range, speed, and size of typical narrow-body regional aircraft. The study is constrained by the ground rules of operating within the current airport and airspace infrastructure. This ongoing study seeks to find a configuration and combination of technologies that yield significant fuel burn and emissions benefits. Another key goal is to reduce cost per passenger mile. Currently, the study is focused on a configuration that utilizes jet A or sustainable aviation fuels, however, we plan to consider other fuel alternatives in the future. This paper describes the progress in defining the architecture of the aircraft, engine, power system, control system, and initial understandings of the sensitivity of the potential configurations to technology assumptions based on key performance parameters. Additionally, progress towards definition and refinement of driving operational, economic, infrastructure, certification, and technical requirements is discussed.</description><language>eng</language><publisher>Glenn Research Center</publisher><subject>Aircraft Design, Testing And Performance</subject><rights>Copyright Determination: GOV_PERMITTED</rights><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><link.rule.ids>309,780,800</link.rule.ids><linktorsrc>$$Uhttps://ntrs.nasa.gov/citations/20220011269$$EView_record_in_NASA$$FView_record_in_$$GNASA$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>Jansen, Ralph H</creatorcontrib><creatorcontrib>Kiris, Cetin C</creatorcontrib><creatorcontrib>Chau, Timothy</creatorcontrib><creatorcontrib>Machado, Leonardo</creatorcontrib><creatorcontrib>Dever, Timothy P</creatorcontrib><creatorcontrib>Litt, Jonathan S</creatorcontrib><creatorcontrib>Arthur, Jarvis J</creatorcontrib><creatorcontrib>Lynde, Michelle N</creatorcontrib><creatorcontrib>Chapman, Jeffryes W</creatorcontrib><creatorcontrib>Kratz, Jonathan L</creatorcontrib><creatorcontrib>Turner, Mark G</creatorcontrib><creatorcontrib>Mirhashemi, Arman</creatorcontrib><creatorcontrib>Denham, Casey L</creatorcontrib><creatorcontrib>Wishart, Jacob M</creatorcontrib><creatorcontrib>Mahavier, Kendall</creatorcontrib><creatorcontrib>Boucher, Matthew J</creatorcontrib><creatorcontrib>Heersema, Nic</creatorcontrib><creatorcontrib>Stalcup, Erik J</creatorcontrib><title>Update on Subsonic Single Aft Engine (SUSAN) Electrofan Trade Space Exploration</title><description>NASA is conducting an ongoing trade study analysis of the SUSAN Electrofan aircraft concept, which utilizes 20-MW-class electrified aircraft propulsion to enable propulsive, aerodynamic, and control benefits while retaining the range, speed, and size of typical narrow-body regional aircraft. The study is constrained by the ground rules of operating within the current airport and airspace infrastructure. This ongoing study seeks to find a configuration and combination of technologies that yield significant fuel burn and emissions benefits. Another key goal is to reduce cost per passenger mile. Currently, the study is focused on a configuration that utilizes jet A or sustainable aviation fuels, however, we plan to consider other fuel alternatives in the future. This paper describes the progress in defining the architecture of the aircraft, engine, power system, control system, and initial understandings of the sensitivity of the potential configurations to technology assumptions based on key performance parameters. Additionally, progress towards definition and refinement of driving operational, economic, infrastructure, certification, and technical requirements is discussed.</description><subject>Aircraft Design, Testing And Performance</subject><fulltext>true</fulltext><rsrctype>conference_proceeding</rsrctype><recordtype>conference_proceeding</recordtype><sourceid>CYI</sourceid><recordid>eNqFybEKwjAQANAsDqL-gcONOghphELHUiJOOqSdy5leSiBcQhLBz3dxd3rD24rnlBasBJHBvF8lsrdgPK-BoHcVNK-eCU5mMv3jDDqQrTk6ZBgzLgQmoSXQnxRixuoj78XGYSh0-LkTx5seh_uFseDMNZdZSaWkbBrVdtc__QU0uDD-</recordid><creator>Jansen, Ralph H</creator><creator>Kiris, Cetin C</creator><creator>Chau, Timothy</creator><creator>Machado, Leonardo</creator><creator>Dever, Timothy P</creator><creator>Litt, Jonathan S</creator><creator>Arthur, Jarvis J</creator><creator>Lynde, Michelle N</creator><creator>Chapman, Jeffryes W</creator><creator>Kratz, Jonathan L</creator><creator>Turner, Mark G</creator><creator>Mirhashemi, Arman</creator><creator>Denham, Casey L</creator><creator>Wishart, Jacob M</creator><creator>Mahavier, Kendall</creator><creator>Boucher, Matthew J</creator><creator>Heersema, Nic</creator><creator>Stalcup, Erik J</creator><scope>CYE</scope><scope>CYI</scope></search><sort><title>Update on Subsonic Single Aft Engine (SUSAN) Electrofan Trade Space Exploration</title><author>Jansen, Ralph H ; Kiris, Cetin C ; Chau, Timothy ; Machado, Leonardo ; Dever, Timothy P ; Litt, Jonathan S ; Arthur, Jarvis J ; Lynde, Michelle N ; Chapman, Jeffryes W ; Kratz, Jonathan L ; Turner, Mark G ; Mirhashemi, Arman ; Denham, Casey L ; Wishart, Jacob M ; Mahavier, Kendall ; Boucher, Matthew J ; Heersema, Nic ; Stalcup, Erik J</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-nasa_ntrs_202200112693</frbrgroupid><rsrctype>conference_proceedings</rsrctype><prefilter>conference_proceedings</prefilter><language>eng</language><topic>Aircraft Design, Testing And Performance</topic><toplevel>online_resources</toplevel><creatorcontrib>Jansen, Ralph H</creatorcontrib><creatorcontrib>Kiris, Cetin C</creatorcontrib><creatorcontrib>Chau, Timothy</creatorcontrib><creatorcontrib>Machado, Leonardo</creatorcontrib><creatorcontrib>Dever, Timothy P</creatorcontrib><creatorcontrib>Litt, Jonathan S</creatorcontrib><creatorcontrib>Arthur, Jarvis J</creatorcontrib><creatorcontrib>Lynde, Michelle N</creatorcontrib><creatorcontrib>Chapman, Jeffryes W</creatorcontrib><creatorcontrib>Kratz, Jonathan L</creatorcontrib><creatorcontrib>Turner, Mark G</creatorcontrib><creatorcontrib>Mirhashemi, Arman</creatorcontrib><creatorcontrib>Denham, Casey L</creatorcontrib><creatorcontrib>Wishart, Jacob M</creatorcontrib><creatorcontrib>Mahavier, Kendall</creatorcontrib><creatorcontrib>Boucher, Matthew J</creatorcontrib><creatorcontrib>Heersema, Nic</creatorcontrib><creatorcontrib>Stalcup, Erik J</creatorcontrib><collection>NASA Scientific and Technical Information</collection><collection>NASA Technical Reports Server</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>Jansen, Ralph H</au><au>Kiris, Cetin C</au><au>Chau, Timothy</au><au>Machado, Leonardo</au><au>Dever, Timothy P</au><au>Litt, Jonathan S</au><au>Arthur, Jarvis J</au><au>Lynde, Michelle N</au><au>Chapman, Jeffryes W</au><au>Kratz, Jonathan L</au><au>Turner, Mark G</au><au>Mirhashemi, Arman</au><au>Denham, Casey L</au><au>Wishart, Jacob M</au><au>Mahavier, Kendall</au><au>Boucher, Matthew J</au><au>Heersema, Nic</au><au>Stalcup, Erik J</au><format>book</format><genre>proceeding</genre><ristype>CONF</ristype><atitle>Update on Subsonic Single Aft Engine (SUSAN) Electrofan Trade Space Exploration</atitle><abstract>NASA is conducting an ongoing trade study analysis of the SUSAN Electrofan aircraft concept, which utilizes 20-MW-class electrified aircraft propulsion to enable propulsive, aerodynamic, and control benefits while retaining the range, speed, and size of typical narrow-body regional aircraft. The study is constrained by the ground rules of operating within the current airport and airspace infrastructure. This ongoing study seeks to find a configuration and combination of technologies that yield significant fuel burn and emissions benefits. Another key goal is to reduce cost per passenger mile. Currently, the study is focused on a configuration that utilizes jet A or sustainable aviation fuels, however, we plan to consider other fuel alternatives in the future. This paper describes the progress in defining the architecture of the aircraft, engine, power system, control system, and initial understandings of the sensitivity of the potential configurations to technology assumptions based on key performance parameters. Additionally, progress towards definition and refinement of driving operational, economic, infrastructure, certification, and technical requirements is discussed.</abstract><cop>Glenn Research Center</cop><oa>free_for_read</oa></addata></record> |
fulltext | fulltext_linktorsrc |
identifier | |
ispartof | |
issn | |
language | eng |
recordid | cdi_nasa_ntrs_20220011269 |
source | NASA Technical Reports Server |
subjects | Aircraft Design, Testing And Performance |
title | Update on Subsonic Single Aft Engine (SUSAN) Electrofan Trade Space Exploration |
url | https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2024-12-26T10%3A36%3A25IST&url_ver=Z39.88-2004&url_ctx_fmt=infofi/fmt:kev:mtx:ctx&rfr_id=info:sid/primo.exlibrisgroup.com:primo3-Article-nasa_CYI&rft_val_fmt=info:ofi/fmt:kev:mtx:book&rft.genre=proceeding&rft.atitle=Update%20on%20Subsonic%20Single%20Aft%20Engine%20(SUSAN)%20Electrofan%20Trade%20Space%20Exploration&rft.au=Jansen,%20Ralph%20H&rft_id=info:doi/&rft_dat=%3Cnasa_CYI%3E20220011269%3C/nasa_CYI%3E%3Curl%3E%3C/url%3E&disable_directlink=true&sfx.directlink=off&sfx.report_link=0&rft_id=info:oai/&rft_id=info:pmid/&rfr_iscdi=true |