About: Vector-R

An Entity of Type: rocket, from Named Graph: http://dbpedia.org, within Data Space: dbpedia.org

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.

Property Value
dbo:MeanOfTransportation/diameter
  • 1.2
dbo:MeanOfTransportation/height
  • 12000.0
dbo:MeanOfTransportation/mass
  • 5000.0
dbo:Rocket/mass
  • 5000.0
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
dbo:diameter
  • 1.200000 (xsd:double)
dbo:failedLaunches
  • 0 (xsd:nonNegativeInteger)
dbo:height
  • 12.000000 (xsd:double)
dbo:launchSite
dbo:manufacturer
dbo:mass
  • 5000000.000000 (xsd:double)
dbo:rocketFunction
dbo:rocketStages
  • 2 (xsd:nonNegativeInteger)
dbo:status
  • Active
dbo:successfulLaunches
  • 2 (xsd:nonNegativeInteger)
dbo:successor
dbo:thumbnail
dbo:totalLaunches
  • 2 (xsd:nonNegativeInteger)
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  • 53563826 (xsd:integer)
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  • 14904 (xsd:nonNegativeInteger)
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  • 1122974360 (xsd:integer)
dbo:wikiPageWikiLink
dbp:comparable
dbp:countryOrigin
  • United States (en)
dbp:cpl
  • 2 (xsd:integer)
dbp:derivatives
dbp:diameter
  • 1.2 m (en)
dbp:fail
  • 0 (xsd:integer)
dbp:family
dbp:function
  • Small satellite launch vehicle (en)
dbp:height
  • 12 m (en)
dbp:launches
  • 2 (xsd:integer)
dbp:manufacturer
dbp:mass
  • 5000.0
dbp:name
  • Vector-R (en)
dbp:sites
dbp:stages
  • 2 (xsd:integer)
dbp:status
  • Active (en)
dbp:success
  • 2 (xsd:integer)
dbp:wikiPageUsesTemplate
dcterms:subject
rdf:type
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
prov:wasDerivedFrom
foaf:depiction
foaf:isPrimaryTopicOf
foaf:name
  • Vector-R (en)
is dbo:maidenFlightRocket of
is dbo:product of
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is dbp:products of
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