Matches in DBpedia 2014 for { <http://dbpedia.org/resource/H-IIB> ?p ?o. }
- H-IIB diameter "5.2".
- H-IIB height "56600.0".
- H-IIB mass "531000.0".
- H-IIB lowerEarthOrbitPayload "19000.0".
- H-IIB mass "531000.0".
- H-IIB abstract "H-IIB (H2B) is an expendable launch system used to launch H-II Transfer Vehicles (HTV, or Kounotori) towards the International Space Station. H-IIB rockets are liquid-fuelled with solid-fuel strap-on boosters and are launched from the Tanegashima Space Center in Japan. Mitsubishi and JAXA have been primarily responsible for design, manufacture, and operation of H-IIB. H-IIB is able to carry a payload of up to 8,000 kg to GTO, compared with the payload of 4,000-6,000 kg for the H-IIA. Its performance to LEO is sufficient for the HTV (16,500 kg). The first H-IIB was launched in September 2009.".
- H-IIB countryOrigin Japan.
- H-IIB diameter "5.2".
- H-IIB height "56.6".
- H-IIB launchSite Tanegashima_Space_Center.
- H-IIB launchSite Yoshinobu_Launch_Complex.
- H-IIB lowerEarthOrbitPayload "1.9E7".
- H-IIB maidenFlight "2009-09-10".
- H-IIB manufacturer Mitsubishi_Heavy_Industries.
- H-IIB mass "5.31E8".
- H-IIB rocketFunction Launch_vehicle.
- H-IIB rocketStages "2".
- H-IIB status "Active".
- H-IIB successfulLaunches "4".
- H-IIB thumbnail H-IIB_F2_launching_HTV2.jpg?width=300.
- H-IIB totalLaunches "4".
- H-IIB wikiPageExternalLink index_e.html.
- H-IIB wikiPageExternalLink abstracte-45-4-16.html.
- H-IIB wikiPageID "2577852".
- H-IIB wikiPageRevisionID "591125423".
- H-IIB altStage2thrust "30798".
- H-IIB boosterengines "1".
- H-IIB boosterfuel Solid-fuel_rocket.
- H-IIB boostername "SRB-A3".
- H-IIB boosters "4".
- H-IIB boosterthrust "9,220kN".
- H-IIB boostertime "114.0".
- H-IIB caption "Liftoff of H-IIB Flight 2".
- H-IIB countryOrigin "Japan".
- H-IIB diameter "5.2 m".
- H-IIB first "2009-09-10".
- H-IIB function Launch_vehicle.
- H-IIB hasPhotoCollection H-IIB.
- H-IIB height "56.6 m".
- H-IIB imsize "250".
- H-IIB launches "4".
- H-IIB leoPayload "19000.0".
- H-IIB manufacturer Mitsubishi_Heavy_Industries.
- H-IIB mass "531000.0".
- H-IIB name "H-IIB".
- H-IIB payload "8000.0".
- H-IIB payloadLocation Geostationary_transfer_orbit.
- H-IIB payloads H-II_Transfer_Vehicle.
- H-IIB sites Tanegashima_Space_Center.
- H-IIB sites Yoshinobu_Launch_Complex.
- H-IIB stage1engines "2".
- H-IIB stage1fuel Liquid_hydrogen.
- H-IIB stage1fuel Liquid_oxygen.
- H-IIB stage1thrust "2,196kN".
- H-IIB stage1time "352.0".
- H-IIB stage2engines "1".
- H-IIB stage2fuel Liquid_hydrogen.
- H-IIB stage2fuel Liquid_oxygen.
- H-IIB stage2thrust "137 kN".
- H-IIB stage2time "499.0".
- H-IIB stages "2".
- H-IIB status "Active".
- H-IIB success "4".
- H-IIB subject Category:Mitsubishi_Heavy_Industries_space_launch_vehicles.
- H-IIB subject Category:Space_launch_vehicles_of_Japan.
- H-IIB type Artifact100021939.
- H-IIB type Conveyance103100490.
- H-IIB type Instrumentality103575240.
- H-IIB type MitsubishiHeavyIndustriesLaunchVehicles.
- H-IIB type Object100002684.
- H-IIB type PhysicalEntity100001930.
- H-IIB type Rocket104099429.
- H-IIB type SpaceLaunchVehiclesOfJapan.
- H-IIB type Vehicle104524313.
- H-IIB type Whole100003553.
- H-IIB type MeanOfTransportation.
- H-IIB type Rocket.
- H-IIB type RocketEngine.
- H-IIB type DesignedArtifact.
- H-IIB comment "H-IIB (H2B) is an expendable launch system used to launch H-II Transfer Vehicles (HTV, or Kounotori) towards the International Space Station. H-IIB rockets are liquid-fuelled with solid-fuel strap-on boosters and are launched from the Tanegashima Space Center in Japan. Mitsubishi and JAXA have been primarily responsible for design, manufacture, and operation of H-IIB. H-IIB is able to carry a payload of up to 8,000 kg to GTO, compared with the payload of 4,000-6,000 kg for the H-IIA.".
- H-IIB label "H-IIB (foguete)".
- H-IIB label "H-IIB".
- H-IIB label "H-IIB".
- H-IIB label "H-IIB".
- H-IIB label "H-IIB".
- H-IIB label "H-IIB".
- H-IIB label "H-IIBロケット".
- H-IIB label "H-IIB運載火箭".
- H-IIB sameAs H-IIB.
- H-IIB sameAs H-IIB.
- H-IIB sameAs H-IIB.
- H-IIB sameAs H-IIBロケット.
- H-IIB sameAs H-IIB.
- H-IIB sameAs H-IIB.
- H-IIB sameAs H-IIB_(foguete).
- H-IIB sameAs m.07p83q.
- H-IIB sameAs Q60580.
- H-IIB sameAs Q60580.
- H-IIB sameAs H-IIB.
- H-IIB wasDerivedFrom H-IIB?oldid=591125423.