Matches in DBpedia 2016-04 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 made its first flight in 2009, and has made a total of five flights through 2015.H-IIB is able to carry a payload of up to 8,000 kilograms (18,000 lb) to GTO, compared with the payload of 4,000-6,000 kg for the H-IIA, a predecessor design. Its performance to LEO is sufficient for the 16,500 kg (36,400 lb) HTV. 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 "5".
- H-IIB thumbnail H-IIB_F2_launching_HTV2.jpg?width=300.
- H-IIB totalLaunches "5".
- H-IIB wikiPageExternalLink h2b-3d.
- H-IIB wikiPageExternalLink index_e.html.
- H-IIB wikiPageExternalLink abstracte-45-4-16.html.
- H-IIB wikiPageID "2577852".
- H-IIB wikiPageLength "12945".
- H-IIB wikiPageOutDegree "85".
- H-IIB wikiPageRevisionID "705205404".
- H-IIB wikiPageWikiLink AAUSAT5.
- H-IIB wikiPageWikiLink Akita_Prefecture.
- H-IIB wikiPageWikiLink ArduSat.
- H-IIB wikiPageWikiLink Battleship_(rocketry).
- H-IIB wikiPageWikiLink Category:Mitsubishi_Heavy_Industries_space_launch_vehicles.
- H-IIB wikiPageWikiLink Category:Space_launch_vehicles_of_Japan.
- H-IIB wikiPageWikiLink Comparison_of_orbital_launch_systems.
- H-IIB wikiPageWikiLink Comparison_of_orbital_launchers_families.
- H-IIB wikiPageWikiLink Coordinated_Universal_Time.
- H-IIB wikiPageWikiLink CubeSat.
- H-IIB wikiPageWikiLink Expendable_launch_system.
- H-IIB wikiPageWikiLink F-1_(satellite).
- H-IIB wikiPageWikiLink Flock-2b.
- H-IIB wikiPageWikiLink GOMX-3.
- H-IIB wikiPageWikiLink Geostationary_transfer_orbit.
- H-IIB wikiPageWikiLink H-IIA.
- H-IIB wikiPageWikiLink H-II_Transfer_Vehicle.
- H-IIB wikiPageWikiLink HTV-1.
- H-IIB wikiPageWikiLink Hydroxyl-terminated_polybutadiene.
- H-IIB wikiPageWikiLink International_Space_Station.
- H-IIB wikiPageWikiLink JAXA.
- H-IIB wikiPageWikiLink Japan.
- H-IIB wikiPageWikiLink Kilogram.
- H-IIB wikiPageWikiLink Kounotori_2.
- H-IIB wikiPageWikiLink Kounotori_3.
- H-IIB wikiPageWikiLink Kounotori_4.
- H-IIB wikiPageWikiLink Kounotori_5.
- H-IIB wikiPageWikiLink LE-5.
- H-IIB wikiPageWikiLink LE-7.
- H-IIB wikiPageWikiLink Launch_vehicle.
- H-IIB wikiPageWikiLink Liquid_hydrogen.
- H-IIB wikiPageWikiLink Liquid_oxygen.
- H-IIB wikiPageWikiLink Low_Earth_orbit.
- H-IIB wikiPageWikiLink Mitsubishi_Heavy_Industries.
- H-IIB wikiPageWikiLink Modular_rocket.
- H-IIB wikiPageWikiLink Niwaka.
- H-IIB wikiPageWikiLink Pico_Dragon.
- H-IIB wikiPageWikiLink Polybutadiene.
- H-IIB wikiPageWikiLink Raiko.
- H-IIB wikiPageWikiLink Rocket.
- H-IIB wikiPageWikiLink S-CUBE.
- H-IIB wikiPageWikiLink SERPENS.
- H-IIB wikiPageWikiLink SRB-A.
- H-IIB wikiPageWikiLink Solid-fuel_rocket.
- H-IIB wikiPageWikiLink Tanegashima.
- H-IIB wikiPageWikiLink Tanegashima_Space_Center.
- H-IIB wikiPageWikiLink TechEdSat.
- H-IIB wikiPageWikiLink TechEdSat-3.
- H-IIB wikiPageWikiLink We-Wish.
- H-IIB wikiPageWikiLink Yoshinobu_Launch_Complex.
- H-IIB wikiPageWikiLink Ōdate.
- H-IIB wikiPageWikiLink File:H-II_series.png.
- H-IIB wikiPageWikiLinkText "H-IIB Launch Vehicle".
- H-IIB wikiPageWikiLinkText "H-IIB Rocket".
- H-IIB wikiPageWikiLinkText "H-IIB rocket".
- H-IIB wikiPageWikiLinkText "H-IIB".
- H-IIB wikiPageWikiLinkText "IIB".
- 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 height "56.6 m".
- H-IIB imsize "250".
- H-IIB launches "5".
- 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.