Orion: Design of a system for assured low-cost human access to space

In recent years, Congress and the American people have begun to seriously question the role and importance of future manned spaceflight. This is mainly due to two factors: a decline in technical competition caused by the collapse of communism, and the high costs associated with the Space Shuttle tra...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Hauptverfasser: Elvander, Josh, Heifetz, Andy, Hunt, Teresa, Zhu, Martin
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 Elvander, Josh
Heifetz, Andy
Hunt, Teresa
Zhu, Martin
description In recent years, Congress and the American people have begun to seriously question the role and importance of future manned spaceflight. This is mainly due to two factors: a decline in technical competition caused by the collapse of communism, and the high costs associated with the Space Shuttle transportation system. With these factors in mind, the ORION system was designed to enable manned spaceflight at a low cost, while maintaining the ability to carry out diverse missions, each with a high degree of flexibility. It is capable of performing satellite servicing missions, supporting a space station via crew rotation and resupply, and delivering satellites into geosynchronous orbit. The components of the system are a primary launch module, an upper stage, and a manned spacecraft capable of dynamic reentry. For satellite servicing and space station resupply missions, the ORION system utilizes three primary modules, an upper stage, and the spacecraft, which is delivered to low earth orbit and used to rendezvous, transfer materials, and make repairs. For launching a geosynchronous satellite, one primary module and an upper stage are used to deliver the satellite, along with an apogee kick motor, into orbit. The system is designed with reusability and modularity in mind in an attempt to lower cost.
format Report
fullrecord <record><control><sourceid>nasa_CYI</sourceid><recordid>TN_cdi_nasa_ntrs_19950006151</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>19950006151</sourcerecordid><originalsourceid>FETCH-nasa_ntrs_199500061513</originalsourceid><addsrcrecordid>eNqFybEKwjAUBdAsDqL-gcP9gUKKVKirVdxc3MsjvmihzZPcFPHvXdydznCWrrvmwdIBnXJ4JFiEgB8WnRAtQ8g56x2jvatgLHjOkyRICEqiGPiSoGu3iDJSNz9Xbns-3Y6XKgmlTyWzr9u28d7v66be_ekvN0Yt6Q</addsrcrecordid><sourcetype>Publisher</sourcetype><iscdi>true</iscdi><recordtype>report</recordtype></control><display><type>report</type><title>Orion: Design of a system for assured low-cost human access to space</title><source>NASA Technical Reports Server</source><creator>Elvander, Josh ; Heifetz, Andy ; Hunt, Teresa ; Zhu, Martin</creator><creatorcontrib>Elvander, Josh ; Heifetz, Andy ; Hunt, Teresa ; Zhu, Martin</creatorcontrib><description>In recent years, Congress and the American people have begun to seriously question the role and importance of future manned spaceflight. This is mainly due to two factors: a decline in technical competition caused by the collapse of communism, and the high costs associated with the Space Shuttle transportation system. With these factors in mind, the ORION system was designed to enable manned spaceflight at a low cost, while maintaining the ability to carry out diverse missions, each with a high degree of flexibility. It is capable of performing satellite servicing missions, supporting a space station via crew rotation and resupply, and delivering satellites into geosynchronous orbit. The components of the system are a primary launch module, an upper stage, and a manned spacecraft capable of dynamic reentry. For satellite servicing and space station resupply missions, the ORION system utilizes three primary modules, an upper stage, and the spacecraft, which is delivered to low earth orbit and used to rendezvous, transfer materials, and make repairs. For launching a geosynchronous satellite, one primary module and an upper stage are used to deliver the satellite, along with an apogee kick motor, into orbit. The system is designed with reusability and modularity in mind in an attempt to lower cost.</description><language>eng</language><publisher>Legacy CDMS</publisher><subject>Spacecraft Design, Testing And Performance</subject><creationdate>1994</creationdate><rights>Copyright Determination: GOV_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/19950006151$$EView_record_in_NASA$$FView_record_in_$$GNASA$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>Elvander, Josh</creatorcontrib><creatorcontrib>Heifetz, Andy</creatorcontrib><creatorcontrib>Hunt, Teresa</creatorcontrib><creatorcontrib>Zhu, Martin</creatorcontrib><title>Orion: Design of a system for assured low-cost human access to space</title><description>In recent years, Congress and the American people have begun to seriously question the role and importance of future manned spaceflight. This is mainly due to two factors: a decline in technical competition caused by the collapse of communism, and the high costs associated with the Space Shuttle transportation system. With these factors in mind, the ORION system was designed to enable manned spaceflight at a low cost, while maintaining the ability to carry out diverse missions, each with a high degree of flexibility. It is capable of performing satellite servicing missions, supporting a space station via crew rotation and resupply, and delivering satellites into geosynchronous orbit. The components of the system are a primary launch module, an upper stage, and a manned spacecraft capable of dynamic reentry. For satellite servicing and space station resupply missions, the ORION system utilizes three primary modules, an upper stage, and the spacecraft, which is delivered to low earth orbit and used to rendezvous, transfer materials, and make repairs. For launching a geosynchronous satellite, one primary module and an upper stage are used to deliver the satellite, along with an apogee kick motor, into orbit. The system is designed with reusability and modularity in mind in an attempt to lower cost.</description><subject>Spacecraft Design, Testing And Performance</subject><fulltext>true</fulltext><rsrctype>report</rsrctype><creationdate>1994</creationdate><recordtype>report</recordtype><sourceid>CYI</sourceid><recordid>eNqFybEKwjAUBdAsDqL-gcP9gUKKVKirVdxc3MsjvmihzZPcFPHvXdydznCWrrvmwdIBnXJ4JFiEgB8WnRAtQ8g56x2jvatgLHjOkyRICEqiGPiSoGu3iDJSNz9Xbns-3Y6XKgmlTyWzr9u28d7v66be_ekvN0Yt6Q</recordid><startdate>19940101</startdate><enddate>19940101</enddate><creator>Elvander, Josh</creator><creator>Heifetz, Andy</creator><creator>Hunt, Teresa</creator><creator>Zhu, Martin</creator><scope>CYE</scope><scope>CYI</scope></search><sort><creationdate>19940101</creationdate><title>Orion: Design of a system for assured low-cost human access to space</title><author>Elvander, Josh ; Heifetz, Andy ; Hunt, Teresa ; Zhu, Martin</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-nasa_ntrs_199500061513</frbrgroupid><rsrctype>reports</rsrctype><prefilter>reports</prefilter><language>eng</language><creationdate>1994</creationdate><topic>Spacecraft Design, Testing And Performance</topic><toplevel>online_resources</toplevel><creatorcontrib>Elvander, Josh</creatorcontrib><creatorcontrib>Heifetz, Andy</creatorcontrib><creatorcontrib>Hunt, Teresa</creatorcontrib><creatorcontrib>Zhu, Martin</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>Elvander, Josh</au><au>Heifetz, Andy</au><au>Hunt, Teresa</au><au>Zhu, Martin</au><format>book</format><genre>unknown</genre><ristype>RPRT</ristype><btitle>Orion: Design of a system for assured low-cost human access to space</btitle><date>1994-01-01</date><risdate>1994</risdate><abstract>In recent years, Congress and the American people have begun to seriously question the role and importance of future manned spaceflight. This is mainly due to two factors: a decline in technical competition caused by the collapse of communism, and the high costs associated with the Space Shuttle transportation system. With these factors in mind, the ORION system was designed to enable manned spaceflight at a low cost, while maintaining the ability to carry out diverse missions, each with a high degree of flexibility. It is capable of performing satellite servicing missions, supporting a space station via crew rotation and resupply, and delivering satellites into geosynchronous orbit. The components of the system are a primary launch module, an upper stage, and a manned spacecraft capable of dynamic reentry. For satellite servicing and space station resupply missions, the ORION system utilizes three primary modules, an upper stage, and the spacecraft, which is delivered to low earth orbit and used to rendezvous, transfer materials, and make repairs. For launching a geosynchronous satellite, one primary module and an upper stage are used to deliver the satellite, along with an apogee kick motor, into orbit. The system is designed with reusability and modularity in mind in an attempt to lower cost.</abstract><cop>Legacy CDMS</cop><oa>free_for_read</oa></addata></record>
fulltext fulltext_linktorsrc
identifier
ispartof
issn
language eng
recordid cdi_nasa_ntrs_19950006151
source NASA Technical Reports Server
subjects Spacecraft Design, Testing And Performance
title Orion: Design of a system for assured low-cost human access to space
url https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-01T18%3A25%3A34IST&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=Orion:%20Design%20of%20a%20system%20for%20assured%20low-cost%20human%20access%20to%20space&rft.au=Elvander,%20Josh&rft.date=1994-01-01&rft_id=info:doi/&rft_dat=%3Cnasa_CYI%3E19950006151%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