Matches in DBpedia 2016-04 for { <http://dbpedia.org/resource/H-II> ?p ?o }
- H-II diameter "4.0".
- H-II height "49000.0".
- H-II mass "260000.0".
- H-II lowerEarthOrbitPayload "10060.0".
- H-II mass "260000.0".
- H-II abstract "The H-II (H2) rocket was a Japanese satellite launch system, which flew seven times between 1994 and 1999, with five successes. It was developed by NASDA in order to give Japan a capability to launch larger satellites in the 1990s. It was the first two-stage liquid-fuelled rocket Japan made using only technologies developed domestically. It was superseded by the H-IIA rocket following reliability and cost issues.".
- H-II countryOrigin Japan.
- H-II diameter "4.0".
- H-II failedLaunches "1".
- H-II finalFlight "1999-11-15".
- H-II height "49.0".
- H-II launchSite Tanegashima_Space_Center.
- H-II launchSite Yoshinobu_Launch_Complex.
- H-II lowerEarthOrbitPayload "1.006E7".
- H-II maidenFlight "1994-02-03".
- H-II manufacturer Mitsubishi_Heavy_Industries.
- H-II mass "2.6E8".
- H-II partialFailedLaunches "1".
- H-II rocketFunction Launch_vehicle.
- H-II rocketStages "2".
- H-II status "Retired".
- H-II successfulLaunches "5".
- H-II thumbnail H-ii_adeos.gif?width=300.
- H-II totalLaunches "7".
- H-II wikiPageExternalLink index_e.html.
- H-II wikiPageID "8519352".
- H-II wikiPageLength "7669".
- H-II wikiPageOutDegree "55".
- H-II wikiPageRevisionID "658962925".
- H-II wikiPageWikiLink ADEOS_I.
- H-II wikiPageWikiLink Ariane_(rocket_family).
- H-II wikiPageWikiLink Category:Mitsubishi_Heavy_Industries_space_launch_vehicles.
- H-II wikiPageWikiLink Category:Space_launch_vehicles_of_Japan.
- H-II wikiPageWikiLink Chichijima.
- H-II wikiPageWikiLink Comparison_of_orbital_launch_systems.
- H-II wikiPageWikiLink Comparison_of_orbital_launchers_families.
- H-II wikiPageWikiLink Coordinated_Universal_Time.
- H-II wikiPageWikiLink DRTS.
- H-II wikiPageWikiLink Delta_(rocket_family).
- H-II wikiPageWikiLink ETS-VII.
- H-II wikiPageWikiLink Geostationary_transfer_orbit.
- H-II wikiPageWikiLink Geosynchronous_orbit.
- H-II wikiPageWikiLink H-I.
- H-II wikiPageWikiLink H-IIA.
- H-II wikiPageWikiLink H-IIB.
- H-II wikiPageWikiLink H-II_(rocket_family).
- H-II wikiPageWikiLink H-II_Transfer_Vehicle.
- H-II wikiPageWikiLink HOPE-X.
- H-II wikiPageWikiLink Himawari_(satellite).
- H-II wikiPageWikiLink Inertial_navigation_system.
- H-II wikiPageWikiLink Japan.
- H-II wikiPageWikiLink LE-5.
- H-II wikiPageWikiLink LE-7.
- H-II wikiPageWikiLink Launch_vehicle.
- H-II wikiPageWikiLink Liquid-propellant_rocket.
- H-II wikiPageWikiLink Liquid_hydrogen.
- H-II wikiPageWikiLink Liquid_oxygen.
- H-II wikiPageWikiLink Low_Earth_orbit.
- H-II wikiPageWikiLink MDS-1.
- H-II wikiPageWikiLink Mitsubishi_Heavy_Industries.
- H-II wikiPageWikiLink Multi-Functional_Transport_Satellite.
- H-II wikiPageWikiLink National_Space_Development_Agency_of_Japan.
- H-II wikiPageWikiLink Newton_(unit).
- H-II wikiPageWikiLink Pound_(mass).
- H-II wikiPageWikiLink Rocket_System_Corporation.
- H-II wikiPageWikiLink Satellite.
- H-II wikiPageWikiLink Solid-fuel_rocket.
- H-II wikiPageWikiLink Tanegashima_Space_Center.
- H-II wikiPageWikiLink Tropical_Rainfall_Measuring_Mission.
- H-II wikiPageWikiLink Tsukuba_Space_Center.
- H-II wikiPageWikiLink United_States.
- H-II wikiPageWikiLink Yoshinobu_Launch_Complex.
- H-II wikiPageWikiLinkText "H-2".
- H-II wikiPageWikiLinkText "H-II rocket".
- H-II wikiPageWikiLinkText "H-II".
- H-II wikiPageWikiLinkText "H-II/SSB".
- H-II wikiPageWikiLinkText "H–2".
- H-II altDiameter "13.1".
- H-II altHeight "160.0".
- H-II altLeo "22170.0".
- H-II altMass "570000.0".
- H-II altPayload "8660.0".
- H-II altStage1thrust "242343".
- H-II altStage2thrust "27313".
- H-II boosterengines "1".
- H-II boosterfuel Solid-fuel_rocket.
- H-II boosters "2".
- H-II boostersi "273.0".
- H-II boosterthrust "1,539.997 kN".
- H-II boostertime "94.0".
- H-II caption "The launch of H-II Flight 4, carrying ADEOS I".
- H-II countryOrigin Japan.
- H-II diameter "4 m".
- H-II fail "1".
- H-II first "1994-02-03".
- H-II function Launch_vehicle.
- H-II height "49 m".
- H-II last "1999-11-15".
- H-II launches "7".
- H-II leoPayload "10060.0".