Matches in DBpedia 2016-04 for { <http://dbpedia.org/resource/N-I_(rocket)> ?p ?o }
- N-I_(rocket) diameter "2.44".
- N-I_(rocket) height "34000.0".
- N-I_(rocket) mass "131330.0".
- N-I_(rocket) mass "131330.0".
- N-I_(rocket) abstract "The N-I or N-1 was a derivative of the American Delta rocket, produced under licence in Japan. It used a Thor-ELT first stage, a Mitsubishi Heavy Industries-designed LE-3 engine was used as a second stage, and three Castor SRMs. Seven were launched between 1975 and 1982, before it was replaced by the N-II. Six of the seven launches were successful, however on the fifth flight, there was recontact between the satellite and the third stage, which caused the satellite to fail.On 29 February 1976, the second N-I conducted the only orbital launch to occur on a leap day (as of year 2008).".
- N-I_(rocket) diameter "2.44".
- N-I_(rocket) finalFlight "1982-09-03".
- N-I_(rocket) height "34.0".
- N-I_(rocket) launchSite Tanegashima.
- N-I_(rocket) maidenFlight "1975-09-09".
- N-I_(rocket) manufacturer Mitsubishi_Heavy_Industries.
- N-I_(rocket) mass "1.3133E8".
- N-I_(rocket) partialFailedLaunches "1".
- N-I_(rocket) rocketFunction Launch_vehicle.
- N-I_(rocket) rocketStages "2".
- N-I_(rocket) rocketStages "3".
- N-I_(rocket) status "Retired".
- N-I_(rocket) successfulLaunches "6".
- N-I_(rocket) thumbnail N-I.svg?width=300.
- N-I_(rocket) totalLaunches "7".
- N-I_(rocket) wikiPageID "19114865".
- N-I_(rocket) wikiPageLength "5712".
- N-I_(rocket) wikiPageOutDegree "57".
- N-I_(rocket) wikiPageRevisionID "705235467".
- N-I_(rocket) wikiPageWikiLink Aerozine_50.
- N-I_(rocket) wikiPageWikiLink Ayame-1.
- N-I_(rocket) wikiPageWikiLink Ayame-2.
- N-I_(rocket) wikiPageWikiLink Castor_(rocket_stage).
- N-I_(rocket) wikiPageWikiLink Category:Mitsubishi_Heavy_Industries_space_launch_vehicles.
- N-I_(rocket) wikiPageWikiLink Category:Space_launch_vehicles_of_Japan.
- N-I_(rocket) wikiPageWikiLink Comparison_of_orbital_launchers_families.
- N-I_(rocket) wikiPageWikiLink Delta_(rocket_family).
- N-I_(rocket) wikiPageWikiLink Dinitrogen_tetroxide.
- N-I_(rocket) wikiPageWikiLink ECS-A.
- N-I_(rocket) wikiPageWikiLink ECS-B.
- N-I_(rocket) wikiPageWikiLink ETS-2.
- N-I_(rocket) wikiPageWikiLink ETS-3.
- N-I_(rocket) wikiPageWikiLink ETS1.
- N-I_(rocket) wikiPageWikiLink February_29.
- N-I_(rocket) wikiPageWikiLink Geostationary_transfer_orbit.
- N-I_(rocket) wikiPageWikiLink H-I.
- N-I_(rocket) wikiPageWikiLink H-II.
- N-I_(rocket) wikiPageWikiLink H-IIA.
- N-I_(rocket) wikiPageWikiLink ISS-1.
- N-I_(rocket) wikiPageWikiLink ISS-2.
- N-I_(rocket) wikiPageWikiLink JETS-1.
- N-I_(rocket) wikiPageWikiLink JISS-1.
- N-I_(rocket) wikiPageWikiLink JISS-2.
- N-I_(rocket) wikiPageWikiLink Kiku-1.
- N-I_(rocket) wikiPageWikiLink Kiku-2.
- N-I_(rocket) wikiPageWikiLink Kiku-3.
- N-I_(rocket) wikiPageWikiLink Launch_vehicle.
- N-I_(rocket) wikiPageWikiLink Liquid_oxygen.
- N-I_(rocket) wikiPageWikiLink Low_Earth_orbit.
- N-I_(rocket) wikiPageWikiLink MB-3-3.
- N-I_(rocket) wikiPageWikiLink Mitsubishi_Heavy_Industries.
- N-I_(rocket) wikiPageWikiLink N-II_(rocket).
- N-I_(rocket) wikiPageWikiLink PGM-17_Thor.
- N-I_(rocket) wikiPageWikiLink RP-1.
- N-I_(rocket) wikiPageWikiLink Solid-fuel_rocket.
- N-I_(rocket) wikiPageWikiLink Star_37.
- N-I_(rocket) wikiPageWikiLink TX-354-3.
- N-I_(rocket) wikiPageWikiLink Tanegashima.
- N-I_(rocket) wikiPageWikiLink Thor_(rocket_family).
- N-I_(rocket) wikiPageWikiLink Ume-1.
- N-I_(rocket) wikiPageWikiLink Ume-2.
- N-I_(rocket) wikiPageWikiLink File:Rocket-Namba.jpg.
- N-I_(rocket) wikiPageWikiLinkText "N-I (rocket)".
- N-I_(rocket) wikiPageWikiLinkText "N-I".
- N-I_(rocket) caption "The N-I rocket".
- N-I_(rocket) countryOrigin "USA".
- N-I_(rocket) family Delta_(rocket_family).
- N-I_(rocket) first "1975-09-09".
- N-I_(rocket) function Launch_vehicle.
- N-I_(rocket) imsize "75".
- N-I_(rocket) last "1982-09-03".
- N-I_(rocket) launches "7".
- N-I_(rocket) manufacturer Mitsubishi_Heavy_Industries.
- N-I_(rocket) name "N-I".
- N-I_(rocket) partial "1".
- N-I_(rocket) sites "LA-N, Tanegashima".
- N-I_(rocket) stages "2".
- N-I_(rocket) status "Retired".
- N-I_(rocket) success "6".
- N-I_(rocket) wikiPageUsesTemplate Template:About.
- N-I_(rocket) wikiPageUsesTemplate Template:Convert.
- N-I_(rocket) wikiPageUsesTemplate Template:Expendable_launch_systems.
- N-I_(rocket) wikiPageUsesTemplate Template:Infobox_Rocket.
- N-I_(rocket) wikiPageUsesTemplate Payload.
- N-I_(rocket) wikiPageUsesTemplate Stage.
- N-I_(rocket) wikiPageUsesTemplate Template:JPN.
- N-I_(rocket) wikiPageUsesTemplate Template:Japanese_launch_systems.
- N-I_(rocket) wikiPageUsesTemplate Template:Mitsubishi_Heavy_Industries.
- N-I_(rocket) wikiPageUsesTemplate Template:Reflist.
- N-I_(rocket) wikiPageUsesTemplate Template:Rocket-stub.
- N-I_(rocket) wikiPageUsesTemplate Template:Thor_and_Delta_rockets.
- N-I_(rocket) wikiPageUsesTemplate Template:Use_dmy_dates.
- N-I_(rocket) subject Category:Mitsubishi_Heavy_Industries_space_launch_vehicles.
- N-I_(rocket) subject Category:Space_launch_vehicles_of_Japan.
- N-I_(rocket) hypernym Derivative.