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- 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) wikiPageRevisionID "545417430".
- 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) hasPhotoCollection N-I_(rocket).
- 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) subject Category:Mitsubishi_Heavy_Industries_space_launch_vehicles.
- N-I_(rocket) subject Category:Space_launch_vehicles_of_Japan.
- N-I_(rocket) type Artifact100021939.
- N-I_(rocket) type Conveyance103100490.
- N-I_(rocket) type Instrumentality103575240.
- N-I_(rocket) type MitsubishiHeavyIndustriesLaunchVehicles.
- N-I_(rocket) type Object100002684.
- N-I_(rocket) type PhysicalEntity100001930.
- N-I_(rocket) type Rocket104099429.
- N-I_(rocket) type SpaceLaunchVehiclesOfJapan.
- N-I_(rocket) type Vehicle104524313.
- N-I_(rocket) type Whole100003553.
- N-I_(rocket) type MeanOfTransportation.
- N-I_(rocket) type Rocket.
- N-I_(rocket) type RocketEngine.
- N-I_(rocket) type DesignedArtifact.
- N-I_(rocket) comment "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.".
- N-I_(rocket) label "N-I (foguete)".
- N-I_(rocket) label "N-I (fusée)".
- N-I_(rocket) label "N-I (rocket)".
- N-I_(rocket) label "N-I (ракета-носитель)".
- N-I_(rocket) label "N-I".
- N-I_(rocket) label "N-Iロケット".
- N-I_(rocket) label "N-I運載火箭".
- N-I_(rocket) sameAs N-I_(fusée).
- N-I_(rocket) sameAs N-I_(roket).
- N-I_(rocket) sameAs N-Iロケット.
- N-I_(rocket) sameAs N-I.
- N-I_(rocket) sameAs N-I.
- N-I_(rocket) sameAs N-I_(foguete).
- N-I_(rocket) sameAs m.04jd3j4.
- N-I_(rocket) sameAs Q618897.
- N-I_(rocket) sameAs Q618897.
- N-I_(rocket) sameAs N-I_(rocket).
- N-I_(rocket) wasDerivedFrom N-I_(rocket)?oldid=545417430.
- N-I_(rocket) depiction N-I.svg.
- N-I_(rocket) isPrimaryTopicOf N-I_(rocket).
- N-I_(rocket) name "N-I".