EARTH TO ORBIT TRANSPORTATION SYSTEM
Various embodiments of space launch vehicle systems and associated methods of manufacture and use are disclosed herein. In some embodiments, the systems include a reusable, horizontal takeoff/horizontal landing (HTML), ground-assisted singie-stage-to-orbit (SSTO) spaceplane that is capable of provid...
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| creator | HOLDER, Livingston HUDSON, Gary MCKINNEY, Bevin CRENSHAW, Marshall |
| description | Various embodiments of space launch vehicle systems and associated methods of manufacture and use are disclosed herein. In some embodiments, the systems include a reusable, horizontal takeoff/horizontal landing (HTML), ground-assisted singie-stage-to-orbit (SSTO) spaceplane that is capable of providing frequent deliveries of people and/or cargo to Low Earth Orbit (LEO). In some embodiments, the spaceplane can takeoff with the aid of a rocket-powered sled that, in addition to providing additional thrust for takeoff, can also provide propellant for the spaceplane engines during the takeoff run so that the spaceplane launches with full propellant tanks.
L'invention concerne divers modes de réalisation de systèmes de lanceur spatial et des procédés de fabrication et d'utilisation associés. Selon certains modes de réalisation, les systèmes comprennent une navette spatiale réutilisable à décollage et atterrissage horizontal (HTML), monoétage à ascension directe (SSTO), à assistance au sol, qui est capable d'assurer des acheminements fréquents de personnes et/ou de chargements à une orbite basse (LEO). Selon certains modes de réalisation, la navette spatiale peut décoller à l'aide d'une luge à réaction qui, en plus de fournir une poussée supplémentaire pour le décollage, peut également fournir du propergol aux moteurs de la navette spatiale pendant la course de décollage de telle sorte que la navette spatiale est lancée avec des réservoirs de propergol pleins. |
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L'invention concerne divers modes de réalisation de systèmes de lanceur spatial et des procédés de fabrication et d'utilisation associés. Selon certains modes de réalisation, les systèmes comprennent une navette spatiale réutilisable à décollage et atterrissage horizontal (HTML), monoétage à ascension directe (SSTO), à assistance au sol, qui est capable d'assurer des acheminements fréquents de personnes et/ou de chargements à une orbite basse (LEO). Selon certains modes de réalisation, la navette spatiale peut décoller à l'aide d'une luge à réaction qui, en plus de fournir une poussée supplémentaire pour le décollage, peut également fournir du propergol aux moteurs de la navette spatiale pendant la course de décollage de telle sorte que la navette spatiale est lancée avec des réservoirs de propergol pleins.</description><language>eng ; fre</language><subject>AIRCRAFT ; AVIATION ; BLASTING ; COSMONAUTICS ; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING ORREPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR ; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED,LIQUEFIED, OR SOLIDIFIED GASES ; FIXED-CAPACITY GAS-HOLDERS ; GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLYADAPTED FOR USE IN CONNECTION WITH AIRCRAFT ; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFTCOMPONENTS, NOT OTHERWISE PROVIDED FOR ; HEATING ; LIGHTING ; MECHANICAL ENGINEERING ; PERFORMING OPERATIONS ; STORING OF DISTRIBUTING GASES OR LIQUIDS ; TRANSPORTING ; VEHICLES OR EQUIPMENT THEREFOR ; VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED ORSOLIDIFIED GASES ; WEAPONS</subject><creationdate>2019</creationdate><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://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20191128&DB=EPODOC&CC=WO&NR=2019227046A1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76547</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20191128&DB=EPODOC&CC=WO&NR=2019227046A1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>HOLDER, Livingston</creatorcontrib><creatorcontrib>HUDSON, Gary</creatorcontrib><creatorcontrib>MCKINNEY, Bevin</creatorcontrib><creatorcontrib>CRENSHAW, Marshall</creatorcontrib><title>EARTH TO ORBIT TRANSPORTATION SYSTEM</title><description>Various embodiments of space launch vehicle systems and associated methods of manufacture and use are disclosed herein. In some embodiments, the systems include a reusable, horizontal takeoff/horizontal landing (HTML), ground-assisted singie-stage-to-orbit (SSTO) spaceplane that is capable of providing frequent deliveries of people and/or cargo to Low Earth Orbit (LEO). In some embodiments, the spaceplane can takeoff with the aid of a rocket-powered sled that, in addition to providing additional thrust for takeoff, can also provide propellant for the spaceplane engines during the takeoff run so that the spaceplane launches with full propellant tanks.
L'invention concerne divers modes de réalisation de systèmes de lanceur spatial et des procédés de fabrication et d'utilisation associés. Selon certains modes de réalisation, les systèmes comprennent une navette spatiale réutilisable à décollage et atterrissage horizontal (HTML), monoétage à ascension directe (SSTO), à assistance au sol, qui est capable d'assurer des acheminements fréquents de personnes et/ou de chargements à une orbite basse (LEO). Selon certains modes de réalisation, la navette spatiale peut décoller à l'aide d'une luge à réaction qui, en plus de fournir une poussée supplémentaire pour le décollage, peut également fournir du propergol aux moteurs de la navette spatiale pendant la course de décollage de telle sorte que la navette spatiale est lancée avec des réservoirs de propergol pleins.</description><subject>AIRCRAFT</subject><subject>AVIATION</subject><subject>BLASTING</subject><subject>COSMONAUTICS</subject><subject>DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING ORREPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR</subject><subject>FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED,LIQUEFIED, OR SOLIDIFIED GASES</subject><subject>FIXED-CAPACITY GAS-HOLDERS</subject><subject>GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLYADAPTED FOR USE IN CONNECTION WITH AIRCRAFT</subject><subject>HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFTCOMPONENTS, NOT OTHERWISE PROVIDED FOR</subject><subject>HEATING</subject><subject>LIGHTING</subject><subject>MECHANICAL ENGINEERING</subject><subject>PERFORMING OPERATIONS</subject><subject>STORING OF DISTRIBUTING GASES OR LIQUIDS</subject><subject>TRANSPORTING</subject><subject>VEHICLES OR EQUIPMENT THEREFOR</subject><subject>VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED ORSOLIDIFIED GASES</subject><subject>WEAPONS</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2019</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZFBxdQwK8VAI8VfwD3LyDFEICXL0Cw7wDwpxDPH091MIjgwOcfXlYWBNS8wpTuWF0twMym6uIc4euqkF-fGpxQWJyal5qSXx4f5GBoaWRkbmBiZmjobGxKkCAClKJEE</recordid><startdate>20191128</startdate><enddate>20191128</enddate><creator>HOLDER, Livingston</creator><creator>HUDSON, Gary</creator><creator>MCKINNEY, Bevin</creator><creator>CRENSHAW, Marshall</creator><scope>EVB</scope></search><sort><creationdate>20191128</creationdate><title>EARTH TO ORBIT TRANSPORTATION SYSTEM</title><author>HOLDER, Livingston ; HUDSON, Gary ; MCKINNEY, Bevin ; CRENSHAW, Marshall</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_WO2019227046A13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; fre</language><creationdate>2019</creationdate><topic>AIRCRAFT</topic><topic>AVIATION</topic><topic>BLASTING</topic><topic>COSMONAUTICS</topic><topic>DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING ORREPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR</topic><topic>FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED,LIQUEFIED, OR SOLIDIFIED GASES</topic><topic>FIXED-CAPACITY GAS-HOLDERS</topic><topic>GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLYADAPTED FOR USE IN CONNECTION WITH AIRCRAFT</topic><topic>HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFTCOMPONENTS, NOT OTHERWISE PROVIDED FOR</topic><topic>HEATING</topic><topic>LIGHTING</topic><topic>MECHANICAL ENGINEERING</topic><topic>PERFORMING OPERATIONS</topic><topic>STORING OF DISTRIBUTING GASES OR LIQUIDS</topic><topic>TRANSPORTING</topic><topic>VEHICLES OR EQUIPMENT THEREFOR</topic><topic>VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED ORSOLIDIFIED GASES</topic><topic>WEAPONS</topic><toplevel>online_resources</toplevel><creatorcontrib>HOLDER, Livingston</creatorcontrib><creatorcontrib>HUDSON, Gary</creatorcontrib><creatorcontrib>MCKINNEY, Bevin</creatorcontrib><creatorcontrib>CRENSHAW, Marshall</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>HOLDER, Livingston</au><au>HUDSON, Gary</au><au>MCKINNEY, Bevin</au><au>CRENSHAW, Marshall</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>EARTH TO ORBIT TRANSPORTATION SYSTEM</title><date>2019-11-28</date><risdate>2019</risdate><abstract>Various embodiments of space launch vehicle systems and associated methods of manufacture and use are disclosed herein. In some embodiments, the systems include a reusable, horizontal takeoff/horizontal landing (HTML), ground-assisted singie-stage-to-orbit (SSTO) spaceplane that is capable of providing frequent deliveries of people and/or cargo to Low Earth Orbit (LEO). In some embodiments, the spaceplane can takeoff with the aid of a rocket-powered sled that, in addition to providing additional thrust for takeoff, can also provide propellant for the spaceplane engines during the takeoff run so that the spaceplane launches with full propellant tanks.
L'invention concerne divers modes de réalisation de systèmes de lanceur spatial et des procédés de fabrication et d'utilisation associés. Selon certains modes de réalisation, les systèmes comprennent une navette spatiale réutilisable à décollage et atterrissage horizontal (HTML), monoétage à ascension directe (SSTO), à assistance au sol, qui est capable d'assurer des acheminements fréquents de personnes et/ou de chargements à une orbite basse (LEO). Selon certains modes de réalisation, la navette spatiale peut décoller à l'aide d'une luge à réaction qui, en plus de fournir une poussée supplémentaire pour le décollage, peut également fournir du propergol aux moteurs de la navette spatiale pendant la course de décollage de telle sorte que la navette spatiale est lancée avec des réservoirs de propergol pleins.</abstract><oa>free_for_read</oa></addata></record> |
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| subjects | AIRCRAFT AVIATION BLASTING COSMONAUTICS DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING ORREPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED,LIQUEFIED, OR SOLIDIFIED GASES FIXED-CAPACITY GAS-HOLDERS GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLYADAPTED FOR USE IN CONNECTION WITH AIRCRAFT HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFTCOMPONENTS, NOT OTHERWISE PROVIDED FOR HEATING LIGHTING MECHANICAL ENGINEERING PERFORMING OPERATIONS STORING OF DISTRIBUTING GASES OR LIQUIDS TRANSPORTING VEHICLES OR EQUIPMENT THEREFOR VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED ORSOLIDIFIED GASES WEAPONS |
| title | EARTH TO ORBIT TRANSPORTATION SYSTEM |
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