| dbo:MeanOfTransportation/diameter |
1.2 (dbd:metre) |
| dbo:MeanOfTransportation/height |
12000.0 (dbd:millimetre) |
| dbo:MeanOfTransportation/mass |
5000.0 (dbd:kilogram) |
| dbo:Rocket/mass |
5000.0 (dbd:kilogram) |
| dbo:abstract |
Die Vector-R (Vector-Rapide) ist ein Trägerraketenprojekt des US-amerikanischen Raumfahrtunternehmens Vector Launch. Sie war ursprünglich für den Start von Nutzlasten bis 60 kg in niedrige Erdumlaufbahnen (LEO) vorgesehen. Außerdem plante Vector Launch die größere Vector-H (Vector-Heavy) mit 290 kg LEO-Nutzlastkapazität. Beide Modelle sollten vom Pacific Spaceport Complex – Alaska (PSCA), dem Mid-Atlantic Regional Spaceport und dem Vandenberg AFB Space Launch Complex 8 (VAFB LC-8) starten. Wegen finanzieller Schwierigkeiten stellte Vector Launch am 9. August 2019 den Betrieb ein. Die Raketenentwicklung wurde verkauft und im Herbst 2020 unter der neuen Eigentümerschaft wieder aufgenommen, zunächst aber nur mit dem Ziel suborbitaler Flüge mit der neuen Vector-S. (de) Vector-R est un lanceur spatial ultra-léger et partiellement réutilisable de la société américaine (en) (ex Vector Space Systems). Son développement a été interrompu par la défaillance financière de son constructeur au cours de l'été 2019. Ce petit lanceur d'environ 6 tonnes était conçu pour placer sur une orbite basse un ou plusieurs nano-satellites ayant une masse totale d'environ 60 kg. Le lanceur comporte deux étages propulsés par des moteurs-fusées à ergols liquides brûlant un mélange de propylène et d'oxygène liquide. (fr) Vector-R (Vector Rapid) is a two-stage orbital expendable launch vehicle under development by the American aerospace company Vector Launch to cover the commercial small satellite launch segment (CubeSats). Vector Launch went bankrupt in December 2019 and re-emerged in October 2020. Two prototypes were launched in 2017. The rocket completed a maiden test flight at low altitude in May 2017. Vector Launch was planning the maiden orbital launch from the Pacific Spaceport Complex in Alaska in 2019, but paused operation in August 2019 due to an uncertain financing situation. An upgraded version of the Vector-R, called the Vector-H (Heavy), is in development as well. (en) |
| dbo:comparable |
dbr:Electron_(rocket) dbr:Falcon_1 dbr:Firefly_Alpha |
| dbo:diameter |
1.200000 (xsd:double) |
| dbo:failedLaunches |
0 (xsd:nonNegativeInteger) |
| dbo:height |
12.000000 (xsd:double) |
| dbo:launchSite |
dbr:Mojave_Air_and_Space_Port dbr:Pacific_Spaceport_Complex_–_Alaska dbr:Spaceport_Camden dbr:Spaceport_Florida_Launch_Complex_46 dbr:Mid-Atlantic_Regional_Spaceport_Launch_Pad_0 |
| dbo:manufacturer |
dbr:Vector_Launch |
| dbo:mass |
5000000.000000 (xsd:double) |
| dbo:rocketFunction |
dbr:Small_satellite |
| dbo:rocketStages |
2 (xsd:nonNegativeInteger) |
| dbo:status |
Active |
| dbo:successfulLaunches |
2 (xsd:nonNegativeInteger) |
| dbo:successor |
dbr:Vector-H |
| dbo:thumbnail |
wiki-commons:Special:FilePath/Vector-R_Diagram.svg?width=300 |
| dbo:totalLaunches |
2 (xsd:nonNegativeInteger) |
| dbo:wikiPageExternalLink |
https://astrodigital.com/ |
| dbo:wikiPageID |
53563826 (xsd:integer) |
| dbo:wikiPageLength |
14904 (xsd:nonNegativeInteger) |
| dbo:wikiPageRevisionID |
1122974360 (xsd:integer) |
| dbo:wikiPageWikiLink |
dbr:Propylene dbr:Delft_University_of_Technology dbr:CubeSat dbr:Vector-H dbr:Vector_Launch dbr:Coordinated_Universal_Time dbr:Sub-orbital_spaceflight dbr:Electron_(rocket) dbr:Mojave_Air_and_Space_Port dbr:2017_in_spaceflight dbr:2018_in_spaceflight dbr:2019_in_spaceflight dbr:Launch_vehicle dbr:Liquid_oxygen dbr:Alaska dbr:Alba_Orbital dbc:Microsatellite_launch_vehicles dbr:Falcon_1 dbr:Firefly_Alpha dbr:Pacific_Spaceport_Complex_–_Alaska dbr:Flight_test dbr:PocketQube dbr:Sun-synchronous_orbit dbr:Spaceport_Camden dbr:Spaceport_Florida_Launch_Complex_46 dbr:Mid-Atlantic_Regional_Spaceport_Launch_Pad_0 dbr:Newton_(unit) dbr:Mid-Atlantic_Regional_Spaceport dbr:Expendable_launch_system dbr:LOX dbr:Low_Earth_orbit dbr:Small-lift_launch_vehicle dbr:Small_satellite dbr:Two-stage-to-orbit dbr:Sun-synchronous dbr:Vector_(rocket_family) dbr:Astro_Digital dbr:LP-1 dbr:Delfi-PQ_1 dbr:LP-2 dbr:Landmapper-HD dbr:Open_Cosmos dbr:Unicorn_2A dbr:File:Kluft-photo-aerial-Mojave-Spaceport-Sept-2009-Img_0227.jpg |
| dbp:comparable |
dbr:Electron_(rocket) dbr:Falcon_1 dbr:Firefly_Alpha |
| dbp:countryOrigin |
United States (en) |
| dbp:cpl |
2 (xsd:integer) |
| dbp:derivatives |
dbr:Vector-H |
| dbp:diameter |
1.2 m (en) |
| dbp:fail |
0 (xsd:integer) |
| dbp:family |
dbr:Vector_(rocket_family) |
| dbp:function |
Small satellite launch vehicle (en) |
| dbp:height |
12 m (en) |
| dbp:launches |
2 (xsd:integer) |
| dbp:manufacturer |
dbr:Vector_Launch |
| dbp:mass |
5000.0 (dbd:kilogram) |
| dbp:name |
Vector-R (en) |
| dbp:sites |
dbr:Mojave_Air_and_Space_Port dbr:Pacific_Spaceport_Complex_–_Alaska dbr:Spaceport_Camden dbr:Spaceport_Florida_Launch_Complex_46 dbr:Mid-Atlantic_Regional_Spaceport_Launch_Pad_0 |
| dbp:stages |
2 (xsd:integer) |
| dbp:status |
Active (en) |
| dbp:success |
2 (xsd:integer) |
| dbp:wikiPageUsesTemplate |
dbt:Abbr dbt:Citation_needed dbt:Convert dbt:Cvt dbt:N/A dbt:Reflist dbt:Short_description dbt:Success dbt:Column dbt:Columns-end dbt:Columns-start dbt:Infobox_rocket/stage dbt:Infobox_rocket/payload dbt:Infobox_rocket dbt:Orbital_launch_systems dbt:US_launch_systems |
| dct:subject |
dbc:Microsatellite_launch_vehicles |
| rdf:type |
owl:Thing dbo:MeanOfTransportation wikidata:Q41291 dbo:Rocket |
| rdfs:comment |
Vector-R est un lanceur spatial ultra-léger et partiellement réutilisable de la société américaine (en) (ex Vector Space Systems). Son développement a été interrompu par la défaillance financière de son constructeur au cours de l'été 2019. Ce petit lanceur d'environ 6 tonnes était conçu pour placer sur une orbite basse un ou plusieurs nano-satellites ayant une masse totale d'environ 60 kg. Le lanceur comporte deux étages propulsés par des moteurs-fusées à ergols liquides brûlant un mélange de propylène et d'oxygène liquide. (fr) Die Vector-R (Vector-Rapide) ist ein Trägerraketenprojekt des US-amerikanischen Raumfahrtunternehmens Vector Launch. Sie war ursprünglich für den Start von Nutzlasten bis 60 kg in niedrige Erdumlaufbahnen (LEO) vorgesehen. Außerdem plante Vector Launch die größere Vector-H (Vector-Heavy) mit 290 kg LEO-Nutzlastkapazität. Beide Modelle sollten vom Pacific Spaceport Complex – Alaska (PSCA), dem Mid-Atlantic Regional Spaceport und dem Vandenberg AFB Space Launch Complex 8 (VAFB LC-8) starten. (de) Vector-R (Vector Rapid) is a two-stage orbital expendable launch vehicle under development by the American aerospace company Vector Launch to cover the commercial small satellite launch segment (CubeSats). Vector Launch went bankrupt in December 2019 and re-emerged in October 2020. Two prototypes were launched in 2017. The rocket completed a maiden test flight at low altitude in May 2017. Vector Launch was planning the maiden orbital launch from the Pacific Spaceport Complex in Alaska in 2019, but paused operation in August 2019 due to an uncertain financing situation. (en) |
| rdfs:label |
Vector-R (en) Vector (Rakete) (de) Vector-R (fr) |
| owl:sameAs |
yago-res:Vector-R wikidata:Vector-R dbpedia-de:Vector-R dbpedia-fr:Vector-R https://global.dbpedia.org/id/2qSBZ |
| prov:wasDerivedFrom |
wikipedia-en:Vector-R?oldid=1122974360&ns=0 |
| foaf:depiction |
wiki-commons:Special:FilePath/Kluft-photo-aerial-Mojave-Spaceport-Sept-2009-Img_0227.jpg wiki-commons:Special:FilePath/Vector-R_Diagram.svg |
| foaf:isPrimaryTopicOf |
wikipedia-en:Vector-R |
| foaf:name |
Vector-R (en) |
| is dbo:maidenFlightRocket of |
dbr:2017_in_spaceflight |
| is dbo:product of |
dbr:Vector_Launch |
| is dbo:wikiPageRedirects of |
dbr:Vector-R_(Rapide) |
| is dbo:wikiPageWikiLink of |
dbr:Rocket_Lab_Electron dbr:List_of_private_spaceflight_companies dbr:Vector-H dbr:Vector_Launch dbr:Virginia_Commercial_Space_Flight_Authority dbr:List_of_orbital_launch_systems dbr:Mojave_Air_and_Space_Port dbr:2017_in_spaceflight dbr:Spaceport_Camden dbr:Mid-Atlantic_Regional_Spaceport_Launch_Pad_0 dbr:Small-lift_launch_vehicle dbr:Vector-R_(Rapide) |
| is dbp:products of |
dbr:Vector_Launch |
| is foaf:primaryTopic of |
wikipedia-en:Vector-R |
