Matches in DBpedia 2015-10 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 wikiPageLength "9363".
- Start-1 wikiPageOutDegree "70".
- Start-1 wikiPageRevisionID "676044161".
- Start-1 wikiPageWikiLink Amateur_radio_satellite.
- Start-1 wikiPageWikiLink Bomber.
- Start-1 wikiPageWikiLink Category:Expendable_space_launch_systems.
- Start-1 wikiPageWikiLink Category:Space_launch_vehicles_of_Russia.
- Start-1 wikiPageWikiLink Comparison_of_orbital_launchers_families.
- Start-1 wikiPageWikiLink Composite_material.
- Start-1 wikiPageWikiLink DigitalGlobe.
- Start-1 wikiPageWikiLink EROS_(satellite).
- Start-1 wikiPageWikiLink Early_Bird_1.
- Start-1 wikiPageWikiLink File:Start-1_rocket_diagram.JPG.
- Start-1 wikiPageWikiLink File:Start_moving_to_launch_big.jpg.
- Start-1 wikiPageWikiLink File:Start_rocket_diagram.jpg.
- Start-1 wikiPageWikiLink GMT.
- Start-1 wikiPageWikiLink Greenwich_Mean_Time.
- Start-1 wikiPageWikiLink Gurwin_(satellite).
- Start-1 wikiPageWikiLink ICBM.
- Start-1 wikiPageWikiLink Intercontinental_ballistic_missile.
- Start-1 wikiPageWikiLink Iran.
- Start-1 wikiPageWikiLink Israel.
- Start-1 wikiPageWikiLink Kilonewton.
- Start-1 wikiPageWikiLink Launch_vehicle.
- Start-1 wikiPageWikiLink Low_Earth_orbit.
- Start-1 wikiPageWikiLink Low_earth_orbit.
- Start-1 wikiPageWikiLink Moscow_Institute_of_Thermal_Technology.
- Start-1 wikiPageWikiLink Newton_(unit).
- Start-1 wikiPageWikiLink Odin_(satellite).
- Start-1 wikiPageWikiLink Plesetsk.
- Start-1 wikiPageWikiLink Plesetsk_Cosmodrome.
- Start-1 wikiPageWikiLink Pound-force.
- Start-1 wikiPageWikiLink Pound_(force).
- Start-1 wikiPageWikiLink Pound_(mass).
- Start-1 wikiPageWikiLink RT-2PM_Topol.
- Start-1 wikiPageWikiLink Russia.
- Start-1 wikiPageWikiLink START_I.
- Start-1 wikiPageWikiLink Sea_of_Okhotsk.
- Start-1 wikiPageWikiLink Solid-fuel_rocket.
- Start-1 wikiPageWikiLink Solid_rocket.
- Start-1 wikiPageWikiLink Soviet_Union.
- Start-1 wikiPageWikiLink Submarine-launched_ballistic_missile.
- Start-1 wikiPageWikiLink Sun-synchronous_orbit.
- Start-1 wikiPageWikiLink Sun_Synchronous_orbit.
- Start-1 wikiPageWikiLink Sun_synchronous_orbit.
- Start-1 wikiPageWikiLink Svobodny_Cosmodrome.
- Start-1 wikiPageWikiLink Transporter_erector_launcher.
- Start-1 wikiPageWikiLink UNAMSAT_A.
- Start-1 wikiPageWikiLink United_States.
- Start-1 wikiPageWikiLink ZAO_Puskovie_Uslugi.
- Start-1 wikiPageWikiLink Zeya_(satellite).
- Start-1 wikiPageWikiLinkText "Start".
- Start-1 wikiPageWikiLinkText "Start-1".
- 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".