Matches in DBpedia 2014 for { <http://dbpedia.org/resource/Start-1> ?p ?o. }
- Start-1 diameter "1.61".
- Start-1 height "22700.0".
- Start-1 mass "47200.0".
- Start-1 lowerEarthOrbitPayload "532.0".
- Start-1 mass "47200.0".
- Start-1 abstract "Start-1 is a Russian satellite launch vehicle based on the RT-2PM Topol, a Soviet intercontinental ballistic missile developed by Moscow Institute of Thermal Technology.".
- Start-1 countryOrigin Russia.
- Start-1 diameter "1.61".
- Start-1 height "22.7".
- Start-1 launchSite Plesetsk_Cosmodrome.
- Start-1 launchSite Svobodny_Cosmodrome.
- Start-1 lowerEarthOrbitPayload "532000.0".
- Start-1 maidenFlight "1993-03-25".
- Start-1 manufacturer Moscow_Institute_of_Thermal_Technology.
- Start-1 mass "4.72E7".
- Start-1 rocketFunction Launch_vehicle.
- Start-1 rocketStages "4".
- Start-1 status "Active".
- Start-1 successfulLaunches "6".
- Start-1 totalLaunches "6".
- Start-1 wikiPageExternalLink start-vI.pdf.
- Start-1 wikiPageExternalLink start-vII.pdf.
- Start-1 wikiPageExternalLink www.puskuslugi.ru.
- Start-1 wikiPageID "6889624".
- Start-1 wikiPageRevisionID "600884548".
- Start-1 altDiameter "5.28".
- Start-1 altHeight "74.4".
- Start-1 altLeo "1393.0".
- Start-1 altMass "104000.0".
- Start-1 altPayload "368.0".
- Start-1 altStage1thrust "220310".
- Start-1 altStage2thrust "110150".
- Start-1 altStage3thrust "55078".
- Start-1 altStage4thrust "2203".
- Start-1 caption "Start-1 launch vehicle lifting off from the Svobodny Cosmodrome".
- Start-1 countryOrigin Russia.
- Start-1 diameter "1.61 m".
- Start-1 first "1993-03-25".
- Start-1 function "Small orbital launch vehicle".
- Start-1 hasPhotoCollection Start-1.
- Start-1 height "22.7 m".
- Start-1 imsize "225".
- Start-1 launches "6".
- Start-1 leoPayload "532.0".
- Start-1 manufacturer Moscow_Institute_of_Thermal_Technology.
- Start-1 mass "47200.0".
- Start-1 name "Start-1".
- Start-1 payload "167.0".
- Start-1 payloadLocation Sun-synchronous_orbit.
- Start-1 sites "LC158, Plesetsk Cosmodrome".
- Start-1 sites "LC5, Svobodny Cosmodrome".
- Start-1 stage1engines "1".
- Start-1 stage1fuel Solid-fuel_rocket.
- Start-1 stage1name "Start-1".
- Start-1 stage1si "263".
- Start-1 stage1thrust "980 kN".
- Start-1 stage1time "60.0".
- Start-1 stage2engines "1".
- Start-1 stage2fuel Solid-fuel_rocket.
- Start-1 stage2name "Start-2".
- Start-1 stage2si "280".
- Start-1 stage2thrust "490 kN".
- Start-1 stage2time "64.0".
- Start-1 stage3engines "1".
- Start-1 stage3fuel Solid-fuel_rocket.
- Start-1 stage3name "Start-3".
- Start-1 stage3si "280".
- Start-1 stage3thrust "245 kN".
- Start-1 stage3time "56.0".
- Start-1 stage4engines "1".
- Start-1 stage4fuel Solid-fuel_rocket.
- Start-1 stage4name "Start-4".
- Start-1 stage4si "295".
- Start-1 stage4thrust "9.8 kN".
- Start-1 stage4time "207.0".
- Start-1 stages "4".
- Start-1 status "Active".
- Start-1 success "6".
- Start-1 subject Category:Expendable_space_launch_systems.
- Start-1 subject Category:Space_launch_vehicles_of_Russia.
- Start-1 type MeanOfTransportation.
- Start-1 type Rocket.
- Start-1 type RocketEngine.
- Start-1 type TransportationDevice_Vehicle.
- Start-1 type DesignedArtifact.
- Start-1 comment "Start-1 is a Russian satellite launch vehicle based on the RT-2PM Topol, a Soviet intercontinental ballistic missile developed by Moscow Institute of Thermal Technology.".
- Start-1 label "Start (Rakete)".
- Start-1 label "Start-1".
- Start-1 label "Start-1".
- Start-1 label "Start-1".
- Start-1 label "Start-1".
- Start-1 label "Старт (ракета-носитель)".
- Start-1 label "スタールト1".
- Start-1 label "起飞号运载火箭".
- Start-1 sameAs Start_(Rakete).
- Start-1 sameAs Start-1.
- Start-1 sameAs Start-1.
- Start-1 sameAs スタールト1.
- Start-1 sameAs Start-1.
- Start-1 sameAs Start-1.