High Head Unshrouded Impeller Pump Stage Technology
A team of engineers at NASA/MSFC and Boeing, Rocketdyne division, are developing unshrouded impeller technologies that will increase payload and decrease cost of future reusable launch vehicles. Using the latest analytical techniques and experimental data, a two-stage unshrouded fuel pump is being d...
Gespeichert in:
| Hauptverfasser: | , , , , , , , |
|---|---|
| Format: | Report |
| 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 | Williams, Robert W. Skelley, Stephen E. Stewart, Eric T. Droege, Alan R. Prueger, George H. Chen, Wei-Chung Williams, Morgan Turner, James E. |
| description | A team of engineers at NASA/MSFC and Boeing, Rocketdyne division, are developing unshrouded impeller technologies that will increase payload and decrease cost of future reusable launch vehicles. Using the latest analytical techniques and experimental data, a two-stage unshrouded fuel pump is being designed that will meet the performance requirements of a three-stage shrouded pump. Benefits of the new pump include lower manufacturing costs, reduced weight, and increased payload to orbit. |
| format | Report |
| fullrecord | <record><control><sourceid>nasa_CYI</sourceid><recordid>TN_cdi_nasa_ntrs_20000109897</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>20000109897</sourcerecordid><originalsourceid>FETCH-nasa_ntrs_200001098973</originalsourceid><addsrcrecordid>eNrjZDD2yEzPUPBITUxRCM0rzijKL01JTVHwzC1IzclJLVIIKM0tUAguSUxPVQhJTc7Iy8_JT6_kYWBNS8wpTuWF0twMMm6uIc4eunmJxYnxeSVFxfFGBkBgaGBpYWluTEAaAOEhJ88</addsrcrecordid><sourcetype>Publisher</sourcetype><iscdi>true</iscdi><recordtype>report</recordtype></control><display><type>report</type><title>High Head Unshrouded Impeller Pump Stage Technology</title><source>NASA Technical Reports Server</source><creator>Williams, Robert W. ; Skelley, Stephen E. ; Stewart, Eric T. ; Droege, Alan R. ; Prueger, George H. ; Chen, Wei-Chung ; Williams, Morgan ; Turner, James E.</creator><creatorcontrib>Williams, Robert W. ; Skelley, Stephen E. ; Stewart, Eric T. ; Droege, Alan R. ; Prueger, George H. ; Chen, Wei-Chung ; Williams, Morgan ; Turner, James E.</creatorcontrib><description>A team of engineers at NASA/MSFC and Boeing, Rocketdyne division, are developing unshrouded impeller technologies that will increase payload and decrease cost of future reusable launch vehicles. Using the latest analytical techniques and experimental data, a two-stage unshrouded fuel pump is being designed that will meet the performance requirements of a three-stage shrouded pump. Benefits of the new pump include lower manufacturing costs, reduced weight, and increased payload to orbit.</description><language>eng</language><publisher>Marshall Space Flight Center</publisher><subject>Mechanical Engineering</subject><creationdate>2000</creationdate><rights>Copyright Determination: PUBLIC_USE_PERMITTED</rights><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><link.rule.ids>780,800,4490</link.rule.ids><linktorsrc>$$Uhttps://ntrs.nasa.gov/citations/20000109897$$EView_record_in_NASA$$FView_record_in_$$GNASA$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>Williams, Robert W.</creatorcontrib><creatorcontrib>Skelley, Stephen E.</creatorcontrib><creatorcontrib>Stewart, Eric T.</creatorcontrib><creatorcontrib>Droege, Alan R.</creatorcontrib><creatorcontrib>Prueger, George H.</creatorcontrib><creatorcontrib>Chen, Wei-Chung</creatorcontrib><creatorcontrib>Williams, Morgan</creatorcontrib><creatorcontrib>Turner, James E.</creatorcontrib><title>High Head Unshrouded Impeller Pump Stage Technology</title><description>A team of engineers at NASA/MSFC and Boeing, Rocketdyne division, are developing unshrouded impeller technologies that will increase payload and decrease cost of future reusable launch vehicles. Using the latest analytical techniques and experimental data, a two-stage unshrouded fuel pump is being designed that will meet the performance requirements of a three-stage shrouded pump. Benefits of the new pump include lower manufacturing costs, reduced weight, and increased payload to orbit.</description><subject>Mechanical Engineering</subject><fulltext>true</fulltext><rsrctype>report</rsrctype><creationdate>2000</creationdate><recordtype>report</recordtype><sourceid>CYI</sourceid><recordid>eNrjZDD2yEzPUPBITUxRCM0rzijKL01JTVHwzC1IzclJLVIIKM0tUAguSUxPVQhJTc7Iy8_JT6_kYWBNS8wpTuWF0twMMm6uIc4eunmJxYnxeSVFxfFGBkBgaGBpYWluTEAaAOEhJ88</recordid><startdate>20000101</startdate><enddate>20000101</enddate><creator>Williams, Robert W.</creator><creator>Skelley, Stephen E.</creator><creator>Stewart, Eric T.</creator><creator>Droege, Alan R.</creator><creator>Prueger, George H.</creator><creator>Chen, Wei-Chung</creator><creator>Williams, Morgan</creator><creator>Turner, James E.</creator><scope>CYE</scope><scope>CYI</scope></search><sort><creationdate>20000101</creationdate><title>High Head Unshrouded Impeller Pump Stage Technology</title><author>Williams, Robert W. ; Skelley, Stephen E. ; Stewart, Eric T. ; Droege, Alan R. ; Prueger, George H. ; Chen, Wei-Chung ; Williams, Morgan ; Turner, James E.</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-nasa_ntrs_200001098973</frbrgroupid><rsrctype>reports</rsrctype><prefilter>reports</prefilter><language>eng</language><creationdate>2000</creationdate><topic>Mechanical Engineering</topic><toplevel>online_resources</toplevel><creatorcontrib>Williams, Robert W.</creatorcontrib><creatorcontrib>Skelley, Stephen E.</creatorcontrib><creatorcontrib>Stewart, Eric T.</creatorcontrib><creatorcontrib>Droege, Alan R.</creatorcontrib><creatorcontrib>Prueger, George H.</creatorcontrib><creatorcontrib>Chen, Wei-Chung</creatorcontrib><creatorcontrib>Williams, Morgan</creatorcontrib><creatorcontrib>Turner, James E.</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>Williams, Robert W.</au><au>Skelley, Stephen E.</au><au>Stewart, Eric T.</au><au>Droege, Alan R.</au><au>Prueger, George H.</au><au>Chen, Wei-Chung</au><au>Williams, Morgan</au><au>Turner, James E.</au><format>book</format><genre>unknown</genre><ristype>RPRT</ristype><btitle>High Head Unshrouded Impeller Pump Stage Technology</btitle><date>2000-01-01</date><risdate>2000</risdate><abstract>A team of engineers at NASA/MSFC and Boeing, Rocketdyne division, are developing unshrouded impeller technologies that will increase payload and decrease cost of future reusable launch vehicles. Using the latest analytical techniques and experimental data, a two-stage unshrouded fuel pump is being designed that will meet the performance requirements of a three-stage shrouded pump. Benefits of the new pump include lower manufacturing costs, reduced weight, and increased payload to orbit.</abstract><cop>Marshall Space Flight Center</cop><oa>free_for_read</oa></addata></record> |
| fulltext | fulltext_linktorsrc |
| identifier | |
| ispartof | |
| issn | |
| language | eng |
| recordid | cdi_nasa_ntrs_20000109897 |
| source | NASA Technical Reports Server |
| subjects | Mechanical Engineering |
| title | High Head Unshrouded Impeller Pump Stage Technology |
| url | https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-06T10%3A32%3A10IST&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=unknown&rft.btitle=High%20Head%20Unshrouded%20Impeller%20Pump%20Stage%20Technology&rft.au=Williams,%20Robert%20W.&rft.date=2000-01-01&rft_id=info:doi/&rft_dat=%3Cnasa_CYI%3E20000109897%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 |