Matches in DBpedia 2016-04 for { <http://dbpedia.org/resource/N-II_(rocket)> ?p ?o }
- N-II_(rocket) diameter "2.44".
- N-II_(rocket) height "35000.0".
- N-II_(rocket) mass "132690.0".
- N-II_(rocket) mass "132690.0".
- N-II_(rocket) abstract "The N-II or N-2 was a derivative of the American Delta rocket, produced under licence in Japan. It used a Thor-ELT first stage, a Delta-F second stage, nine Castor SRMs, and on most flights either a Star-37E or Burner-2 upper stage, identical to the US Delta 0100 series configurations. Eight were launched between 1981 and 1987, before it was replaced by the H-I, which featured Japanese-produced upper stages. All eight launches were successful.".
- N-II_(rocket) diameter "2.44".
- N-II_(rocket) finalFlight "1987-02-19".
- N-II_(rocket) height "35.0".
- N-II_(rocket) launchSite Tanegashima.
- N-II_(rocket) maidenFlight "1981-02-11".
- N-II_(rocket) manufacturer Mitsubishi_Heavy_Industries.
- N-II_(rocket) mass "1.3269E8".
- N-II_(rocket) rocketFunction Launch_vehicle.
- N-II_(rocket) rocketStages "2".
- N-II_(rocket) rocketStages "3".
- N-II_(rocket) status "Retired".
- N-II_(rocket) successfulLaunches "8".
- N-II_(rocket) thumbnail N-II.svg?width=300.
- N-II_(rocket) totalLaunches "8".
- N-II_(rocket) wikiPageID "19121539".
- N-II_(rocket) wikiPageLength "4611".
- N-II_(rocket) wikiPageOutDegree "65".
- N-II_(rocket) wikiPageRevisionID "686476475".
- N-II_(rocket) wikiPageWikiLink AJ10.
- N-II_(rocket) wikiPageWikiLink BS-2A.
- N-II_(rocket) wikiPageWikiLink BS-2B.
- N-II_(rocket) wikiPageWikiLink Burner_(rocket_stage).
- N-II_(rocket) wikiPageWikiLink CS-2A.
- N-II_(rocket) wikiPageWikiLink CS-2B.
- N-II_(rocket) wikiPageWikiLink Castor_(rocket_stage).
- N-II_(rocket) wikiPageWikiLink Category:Mitsubishi_Heavy_Industries_space_launch_vehicles.
- N-II_(rocket) wikiPageWikiLink Category:Space_launch_vehicles_of_Japan.
- N-II_(rocket) wikiPageWikiLink Comparison_of_orbital_launchers_families.
- N-II_(rocket) wikiPageWikiLink Delta_(rocket_family).
- N-II_(rocket) wikiPageWikiLink Delta_(rocket_stage).
- N-II_(rocket) wikiPageWikiLink ETS-4.
- N-II_(rocket) wikiPageWikiLink Geostationary_transfer_orbit.
- N-II_(rocket) wikiPageWikiLink H-I.
- N-II_(rocket) wikiPageWikiLink H-II.
- N-II_(rocket) wikiPageWikiLink H-IIA.
- N-II_(rocket) wikiPageWikiLink Himawari-2.
- N-II_(rocket) wikiPageWikiLink Himawari-3.
- N-II_(rocket) wikiPageWikiLink Himawari_(satellite).
- N-II_(rocket) wikiPageWikiLink Japan.
- N-II_(rocket) wikiPageWikiLink Kiku-3.
- N-II_(rocket) wikiPageWikiLink Launch_vehicle.
- N-II_(rocket) wikiPageWikiLink Liquid_oxygen.
- N-II_(rocket) wikiPageWikiLink Low_Earth_orbit.
- N-II_(rocket) wikiPageWikiLink MB-3-3.
- N-II_(rocket) wikiPageWikiLink Medium_Earth_orbit.
- N-II_(rocket) wikiPageWikiLink Mitsubishi_Heavy_Industries.
- N-II_(rocket) wikiPageWikiLink Momo-1.
- N-II_(rocket) wikiPageWikiLink N-I_(rocket).
- N-II_(rocket) wikiPageWikiLink Newark–Elizabeth_Rail_Link.
- N-II_(rocket) wikiPageWikiLink Nitric_acid.
- N-II_(rocket) wikiPageWikiLink PGM-17_Thor.
- N-II_(rocket) wikiPageWikiLink RP-1.
- N-II_(rocket) wikiPageWikiLink Sakura-2A.
- N-II_(rocket) wikiPageWikiLink Sakura-2B.
- N-II_(rocket) wikiPageWikiLink Solid-fuel_rocket.
- N-II_(rocket) wikiPageWikiLink Star_37.
- N-II_(rocket) wikiPageWikiLink TX-354-3.
- N-II_(rocket) wikiPageWikiLink Tanegashima.
- N-II_(rocket) wikiPageWikiLink Thor_(rocket_family).
- N-II_(rocket) wikiPageWikiLink United_States.
- N-II_(rocket) wikiPageWikiLink Unsymmetrical_dimethylhydrazine.
- N-II_(rocket) wikiPageWikiLink Yuri-2A.
- N-II_(rocket) wikiPageWikiLink Yuri-2B.
- N-II_(rocket) wikiPageWikiLinkText "II".
- N-II_(rocket) wikiPageWikiLinkText "N-II (rocket)".
- N-II_(rocket) wikiPageWikiLinkText "N-II".
- N-II_(rocket) caption "The N-II rocket".
- N-II_(rocket) family Delta_(rocket_family).
- N-II_(rocket) first "1981-02-11".
- N-II_(rocket) function Launch_vehicle.
- N-II_(rocket) imsize "75".
- N-II_(rocket) last "1987-02-19".
- N-II_(rocket) launches "8".
- N-II_(rocket) manufacturer Mitsubishi_Heavy_Industries.
- N-II_(rocket) sites "LA-N, Tanegashima".
- N-II_(rocket) stages "2".
- N-II_(rocket) status "Retired".
- N-II_(rocket) success "8".
- N-II_(rocket) wikiPageUsesTemplate Template:Cite_web.
- N-II_(rocket) wikiPageUsesTemplate Template:Convert.
- N-II_(rocket) wikiPageUsesTemplate Template:Expendable_launch_systems.
- N-II_(rocket) wikiPageUsesTemplate Template:Infobox_Rocket.
- N-II_(rocket) wikiPageUsesTemplate Payload.
- N-II_(rocket) wikiPageUsesTemplate Stage.
- N-II_(rocket) wikiPageUsesTemplate Template:JPN.
- N-II_(rocket) wikiPageUsesTemplate Template:Japanese_launch_systems.
- N-II_(rocket) wikiPageUsesTemplate Template:Mitsubishi_Heavy_Industries.
- N-II_(rocket) wikiPageUsesTemplate Template:Rocket-stub.
- N-II_(rocket) wikiPageUsesTemplate Template:Thor_and_Delta_rockets.
- N-II_(rocket) wikiPageUsesTemplate Template:USA.
- N-II_(rocket) subject Category:Mitsubishi_Heavy_Industries_space_launch_vehicles.
- N-II_(rocket) subject Category:Space_launch_vehicles_of_Japan.
- N-II_(rocket) hypernym Derivative.
- N-II_(rocket) type ChemicalSubstance.
- N-II_(rocket) type MeanOfTransportation.