THE FIRST STAGE OF THE SATELLITE CARRIER DROPPABLE FROM THE PLATFORM AIRCRAFT, WHICH IS A TWIN-BOOM WINGED AIR VEHICLE
The invention relates to the aerospace industry, in particular to systems for carrying out payloads into the low Earth orbits.The object of the patent is the first stage (6) of the satellite carrier (2), which is dropped from the platform aircraft (1) and provides the second stage (4) with the fligh...
Gespeichert in:
| Hauptverfasser: | , , , , |
|---|---|
| Format: | Patent |
| Sprache: | eng ; lav |
| 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 | PANOVA, Natalia KUĻEŠOVS, Nikolajs BLUMBERGS, Ilmārs ŠESTAKOVS, Vladimirs KRAVCHENKO, Sergey |
| description | The invention relates to the aerospace industry, in particular to systems for carrying out payloads into the low Earth orbits.The object of the patent is the first stage (6) of the satellite carrier (2), which is dropped from the platform aircraft (1) and provides the second stage (4) with the flight parameters necessary to launch the payload into low Earth orbit. The first stage (6) of the carrier is made in the form of a twin-boom winged air vehicle, which allows placing the payload between its booms (10a) and (10b) under the wing-fuselage (8). The first stage is attached to the platform aircraft (1) using a quick release mechanism (11) and is dropped from the platform aircraft (1) when it reaches a point with specific geographic coordinates and flight parameters. The platform aircraft (1) solves this problem more successfully than the rocket launch vehicle, due to the use of aerodynamic forces. These advantages are also inherent in the first (6) stage of the satellite carrier (2) since it has the ability to use atmospheric oxygen and aerodynamic forces. The ability to use the space between the two booms (10a) and (10b) of twin-boom structures also allows the first stage to lift heavier, larger payloads.
Izgudrojums attiecas uz aviācijas un kosmosa nozari, īpaši uz sistēmām, kas paredzētas derīgo kravu (satelītu) pacelšanai zemajās Zemes orbītās.Izgudrojums ir satelīta nesēja (2) pirmā pakāpe (6), kas tiek atdalīta no lidmašīnas-platformas (1) un nodrošina otrai pakāpei (4) lidojuma parametrus, kas nepieciešami satelītu palaišanai zemajā Zemes orbītā. Satelītu nesēja (2) pirmā pakāpe (6) ir izgatavota kā virsskaņas divkorpusu spārnots lidaparāts (6), kas ļauj novietot derīgo kravu starp tā korpusiem (10a) un (10b) zem spārna-fizelāžas (8). Pirmā pakāpe stiprinās pie lidmašīnas-platformas (1) ar ātrās atdalīšanas mehānisma (11) palīdzību un atdalās no tā, kad lidmašīna-platforma (1) sasniedz punktu ar noteiktām ģeogrāfiskām koordinātām un lidojuma parametriem. Lidmašīna-platforma (1) šo uzdevumu risina veiksmīgāk nekā nesējraķete, jo izmanto aerodinamiskos spēkus. Šīs priekšrocības ir raksturīgas arī satelītu nesēja (2) pirmajai pakāpei (6), jo tai ir iespēja izmantot atmosfēras skābekli un aerodinamiskos spēkus. Iespēja izmantot telpu starp abiem korpusiem (10a) un (10b) divu korpusu konstrukcijās ļauj arī satelītu nesēja (2) pirmajai pakāpei (6) Zemes orbītā ievadīt masīvākus satelītus ar lielākiem izmēriem. |
| format | Patent |
| fullrecord | <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_LV15680A</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>LV15680A</sourcerecordid><originalsourceid>FETCH-epo_espacenet_LV15680A3</originalsourceid><addsrcrecordid>eNqFysEKwjAQBNBePIj6CcJ-gAVFFK_bdNMEoimbpT2WIvEkWqj4_abi3dMMM2-evcUQaMtBIAhWBF7DNAUUcs4KgUJmSwwl-7rGwiXO_vxFtUPRns-AlhWjlg20xioDNgCCtPaSFz7ZVCoqJwUNJeBomc1u_X2Mq18usrUmUSaPw7OL49Bf4yO-OtfsDsfTFvf__g8OWDcy</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>THE FIRST STAGE OF THE SATELLITE CARRIER DROPPABLE FROM THE PLATFORM AIRCRAFT, WHICH IS A TWIN-BOOM WINGED AIR VEHICLE</title><source>esp@cenet</source><creator>PANOVA, Natalia ; KUĻEŠOVS, Nikolajs ; BLUMBERGS, Ilmārs ; ŠESTAKOVS, Vladimirs ; KRAVCHENKO, Sergey</creator><creatorcontrib>PANOVA, Natalia ; KUĻEŠOVS, Nikolajs ; BLUMBERGS, Ilmārs ; ŠESTAKOVS, Vladimirs ; KRAVCHENKO, Sergey</creatorcontrib><description>The invention relates to the aerospace industry, in particular to systems for carrying out payloads into the low Earth orbits.The object of the patent is the first stage (6) of the satellite carrier (2), which is dropped from the platform aircraft (1) and provides the second stage (4) with the flight parameters necessary to launch the payload into low Earth orbit. The first stage (6) of the carrier is made in the form of a twin-boom winged air vehicle, which allows placing the payload between its booms (10a) and (10b) under the wing-fuselage (8). The first stage is attached to the platform aircraft (1) using a quick release mechanism (11) and is dropped from the platform aircraft (1) when it reaches a point with specific geographic coordinates and flight parameters. The platform aircraft (1) solves this problem more successfully than the rocket launch vehicle, due to the use of aerodynamic forces. These advantages are also inherent in the first (6) stage of the satellite carrier (2) since it has the ability to use atmospheric oxygen and aerodynamic forces. The ability to use the space between the two booms (10a) and (10b) of twin-boom structures also allows the first stage to lift heavier, larger payloads.
Izgudrojums attiecas uz aviācijas un kosmosa nozari, īpaši uz sistēmām, kas paredzētas derīgo kravu (satelītu) pacelšanai zemajās Zemes orbītās.Izgudrojums ir satelīta nesēja (2) pirmā pakāpe (6), kas tiek atdalīta no lidmašīnas-platformas (1) un nodrošina otrai pakāpei (4) lidojuma parametrus, kas nepieciešami satelītu palaišanai zemajā Zemes orbītā. Satelītu nesēja (2) pirmā pakāpe (6) ir izgatavota kā virsskaņas divkorpusu spārnots lidaparāts (6), kas ļauj novietot derīgo kravu starp tā korpusiem (10a) un (10b) zem spārna-fizelāžas (8). Pirmā pakāpe stiprinās pie lidmašīnas-platformas (1) ar ātrās atdalīšanas mehānisma (11) palīdzību un atdalās no tā, kad lidmašīna-platforma (1) sasniedz punktu ar noteiktām ģeogrāfiskām koordinātām un lidojuma parametriem. Lidmašīna-platforma (1) šo uzdevumu risina veiksmīgāk nekā nesējraķete, jo izmanto aerodinamiskos spēkus. Šīs priekšrocības ir raksturīgas arī satelītu nesēja (2) pirmajai pakāpei (6), jo tai ir iespēja izmantot atmosfēras skābekli un aerodinamiskos spēkus. Iespēja izmantot telpu starp abiem korpusiem (10a) un (10b) divu korpusu konstrukcijās ļauj arī satelītu nesēja (2) pirmajai pakāpei (6) Zemes orbītā ievadīt masīvākus satelītus ar lielākiem izmēriem.</description><language>eng ; lav</language><subject>AIRCRAFT ; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT ; AVIATION ; COSMONAUTICS ; EQUIPMENT FOR FITTING IN OR TO AIRCRAFT ; FLYING SUITS ; PARACHUTES ; PERFORMING OPERATIONS ; TRANSPORTING ; VEHICLES OR EQUIPMENT THEREFOR</subject><creationdate>2022</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=20221020&DB=EPODOC&CC=LV&NR=15680A$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25544,76293</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20221020&DB=EPODOC&CC=LV&NR=15680A$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>PANOVA, Natalia</creatorcontrib><creatorcontrib>KUĻEŠOVS, Nikolajs</creatorcontrib><creatorcontrib>BLUMBERGS, Ilmārs</creatorcontrib><creatorcontrib>ŠESTAKOVS, Vladimirs</creatorcontrib><creatorcontrib>KRAVCHENKO, Sergey</creatorcontrib><title>THE FIRST STAGE OF THE SATELLITE CARRIER DROPPABLE FROM THE PLATFORM AIRCRAFT, WHICH IS A TWIN-BOOM WINGED AIR VEHICLE</title><description>The invention relates to the aerospace industry, in particular to systems for carrying out payloads into the low Earth orbits.The object of the patent is the first stage (6) of the satellite carrier (2), which is dropped from the platform aircraft (1) and provides the second stage (4) with the flight parameters necessary to launch the payload into low Earth orbit. The first stage (6) of the carrier is made in the form of a twin-boom winged air vehicle, which allows placing the payload between its booms (10a) and (10b) under the wing-fuselage (8). The first stage is attached to the platform aircraft (1) using a quick release mechanism (11) and is dropped from the platform aircraft (1) when it reaches a point with specific geographic coordinates and flight parameters. The platform aircraft (1) solves this problem more successfully than the rocket launch vehicle, due to the use of aerodynamic forces. These advantages are also inherent in the first (6) stage of the satellite carrier (2) since it has the ability to use atmospheric oxygen and aerodynamic forces. The ability to use the space between the two booms (10a) and (10b) of twin-boom structures also allows the first stage to lift heavier, larger payloads.
Izgudrojums attiecas uz aviācijas un kosmosa nozari, īpaši uz sistēmām, kas paredzētas derīgo kravu (satelītu) pacelšanai zemajās Zemes orbītās.Izgudrojums ir satelīta nesēja (2) pirmā pakāpe (6), kas tiek atdalīta no lidmašīnas-platformas (1) un nodrošina otrai pakāpei (4) lidojuma parametrus, kas nepieciešami satelītu palaišanai zemajā Zemes orbītā. Satelītu nesēja (2) pirmā pakāpe (6) ir izgatavota kā virsskaņas divkorpusu spārnots lidaparāts (6), kas ļauj novietot derīgo kravu starp tā korpusiem (10a) un (10b) zem spārna-fizelāžas (8). Pirmā pakāpe stiprinās pie lidmašīnas-platformas (1) ar ātrās atdalīšanas mehānisma (11) palīdzību un atdalās no tā, kad lidmašīna-platforma (1) sasniedz punktu ar noteiktām ģeogrāfiskām koordinātām un lidojuma parametriem. Lidmašīna-platforma (1) šo uzdevumu risina veiksmīgāk nekā nesējraķete, jo izmanto aerodinamiskos spēkus. Šīs priekšrocības ir raksturīgas arī satelītu nesēja (2) pirmajai pakāpei (6), jo tai ir iespēja izmantot atmosfēras skābekli un aerodinamiskos spēkus. Iespēja izmantot telpu starp abiem korpusiem (10a) un (10b) divu korpusu konstrukcijās ļauj arī satelītu nesēja (2) pirmajai pakāpei (6) Zemes orbītā ievadīt masīvākus satelītus ar lielākiem izmēriem.</description><subject>AIRCRAFT</subject><subject>ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT</subject><subject>AVIATION</subject><subject>COSMONAUTICS</subject><subject>EQUIPMENT FOR FITTING IN OR TO AIRCRAFT</subject><subject>FLYING SUITS</subject><subject>PARACHUTES</subject><subject>PERFORMING OPERATIONS</subject><subject>TRANSPORTING</subject><subject>VEHICLES OR EQUIPMENT THEREFOR</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2022</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNqFysEKwjAQBNBePIj6CcJ-gAVFFK_bdNMEoimbpT2WIvEkWqj4_abi3dMMM2-evcUQaMtBIAhWBF7DNAUUcs4KgUJmSwwl-7rGwiXO_vxFtUPRns-AlhWjlg20xioDNgCCtPaSFz7ZVCoqJwUNJeBomc1u_X2Mq18usrUmUSaPw7OL49Bf4yO-OtfsDsfTFvf__g8OWDcy</recordid><startdate>20221020</startdate><enddate>20221020</enddate><creator>PANOVA, Natalia</creator><creator>KUĻEŠOVS, Nikolajs</creator><creator>BLUMBERGS, Ilmārs</creator><creator>ŠESTAKOVS, Vladimirs</creator><creator>KRAVCHENKO, Sergey</creator><scope>EVB</scope></search><sort><creationdate>20221020</creationdate><title>THE FIRST STAGE OF THE SATELLITE CARRIER DROPPABLE FROM THE PLATFORM AIRCRAFT, WHICH IS A TWIN-BOOM WINGED AIR VEHICLE</title><author>PANOVA, Natalia ; KUĻEŠOVS, Nikolajs ; BLUMBERGS, Ilmārs ; ŠESTAKOVS, Vladimirs ; KRAVCHENKO, Sergey</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_LV15680A3</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; lav</language><creationdate>2022</creationdate><topic>AIRCRAFT</topic><topic>ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT</topic><topic>AVIATION</topic><topic>COSMONAUTICS</topic><topic>EQUIPMENT FOR FITTING IN OR TO AIRCRAFT</topic><topic>FLYING SUITS</topic><topic>PARACHUTES</topic><topic>PERFORMING OPERATIONS</topic><topic>TRANSPORTING</topic><topic>VEHICLES OR EQUIPMENT THEREFOR</topic><toplevel>online_resources</toplevel><creatorcontrib>PANOVA, Natalia</creatorcontrib><creatorcontrib>KUĻEŠOVS, Nikolajs</creatorcontrib><creatorcontrib>BLUMBERGS, Ilmārs</creatorcontrib><creatorcontrib>ŠESTAKOVS, Vladimirs</creatorcontrib><creatorcontrib>KRAVCHENKO, Sergey</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>PANOVA, Natalia</au><au>KUĻEŠOVS, Nikolajs</au><au>BLUMBERGS, Ilmārs</au><au>ŠESTAKOVS, Vladimirs</au><au>KRAVCHENKO, Sergey</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>THE FIRST STAGE OF THE SATELLITE CARRIER DROPPABLE FROM THE PLATFORM AIRCRAFT, WHICH IS A TWIN-BOOM WINGED AIR VEHICLE</title><date>2022-10-20</date><risdate>2022</risdate><abstract>The invention relates to the aerospace industry, in particular to systems for carrying out payloads into the low Earth orbits.The object of the patent is the first stage (6) of the satellite carrier (2), which is dropped from the platform aircraft (1) and provides the second stage (4) with the flight parameters necessary to launch the payload into low Earth orbit. The first stage (6) of the carrier is made in the form of a twin-boom winged air vehicle, which allows placing the payload between its booms (10a) and (10b) under the wing-fuselage (8). The first stage is attached to the platform aircraft (1) using a quick release mechanism (11) and is dropped from the platform aircraft (1) when it reaches a point with specific geographic coordinates and flight parameters. The platform aircraft (1) solves this problem more successfully than the rocket launch vehicle, due to the use of aerodynamic forces. These advantages are also inherent in the first (6) stage of the satellite carrier (2) since it has the ability to use atmospheric oxygen and aerodynamic forces. The ability to use the space between the two booms (10a) and (10b) of twin-boom structures also allows the first stage to lift heavier, larger payloads.
Izgudrojums attiecas uz aviācijas un kosmosa nozari, īpaši uz sistēmām, kas paredzētas derīgo kravu (satelītu) pacelšanai zemajās Zemes orbītās.Izgudrojums ir satelīta nesēja (2) pirmā pakāpe (6), kas tiek atdalīta no lidmašīnas-platformas (1) un nodrošina otrai pakāpei (4) lidojuma parametrus, kas nepieciešami satelītu palaišanai zemajā Zemes orbītā. Satelītu nesēja (2) pirmā pakāpe (6) ir izgatavota kā virsskaņas divkorpusu spārnots lidaparāts (6), kas ļauj novietot derīgo kravu starp tā korpusiem (10a) un (10b) zem spārna-fizelāžas (8). Pirmā pakāpe stiprinās pie lidmašīnas-platformas (1) ar ātrās atdalīšanas mehānisma (11) palīdzību un atdalās no tā, kad lidmašīna-platforma (1) sasniedz punktu ar noteiktām ģeogrāfiskām koordinātām un lidojuma parametriem. Lidmašīna-platforma (1) šo uzdevumu risina veiksmīgāk nekā nesējraķete, jo izmanto aerodinamiskos spēkus. Šīs priekšrocības ir raksturīgas arī satelītu nesēja (2) pirmajai pakāpei (6), jo tai ir iespēja izmantot atmosfēras skābekli un aerodinamiskos spēkus. Iespēja izmantot telpu starp abiem korpusiem (10a) un (10b) divu korpusu konstrukcijās ļauj arī satelītu nesēja (2) pirmajai pakāpei (6) Zemes orbītā ievadīt masīvākus satelītus ar lielākiem izmēriem.</abstract><oa>free_for_read</oa></addata></record> |
| fulltext | fulltext_linktorsrc |
| identifier | |
| ispartof | |
| issn | |
| language | eng ; lav |
| recordid | cdi_epo_espacenet_LV15680A |
| source | esp@cenet |
| subjects | AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION COSMONAUTICS EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS PARACHUTES PERFORMING OPERATIONS TRANSPORTING VEHICLES OR EQUIPMENT THEREFOR |
| title | THE FIRST STAGE OF THE SATELLITE CARRIER DROPPABLE FROM THE PLATFORM AIRCRAFT, WHICH IS A TWIN-BOOM WINGED AIR VEHICLE |
| url | https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-27T10%3A58%3A43IST&url_ver=Z39.88-2004&url_ctx_fmt=infofi/fmt:kev:mtx:ctx&rfr_id=info:sid/primo.exlibrisgroup.com:primo3-Article-epo_EVB&rft_val_fmt=info:ofi/fmt:kev:mtx:patent&rft.genre=patent&rft.au=PANOVA,%20Natalia&rft.date=2022-10-20&rft_id=info:doi/&rft_dat=%3Cepo_EVB%3ELV15680A%3C/epo_EVB%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 |