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- 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) wikiPageRevisionID "541448503".
- 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) hasPhotoCollection N-II_(rocket).
- 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) subject Category:Mitsubishi_Heavy_Industries_space_launch_vehicles.
- N-II_(rocket) subject Category:Space_launch_vehicles_of_Japan.
- N-II_(rocket) type Artifact100021939.
- N-II_(rocket) type Conveyance103100490.
- N-II_(rocket) type Instrumentality103575240.
- N-II_(rocket) type MitsubishiHeavyIndustriesLaunchVehicles.
- N-II_(rocket) type Object100002684.
- N-II_(rocket) type PhysicalEntity100001930.
- N-II_(rocket) type Rocket104099429.
- N-II_(rocket) type SpaceLaunchVehiclesOfJapan.
- N-II_(rocket) type Vehicle104524313.
- N-II_(rocket) type Whole100003553.
- N-II_(rocket) type MeanOfTransportation.
- N-II_(rocket) type Rocket.
- N-II_(rocket) type RocketEngine.
- N-II_(rocket) type DesignedArtifact.
- N-II_(rocket) comment "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) label "N-II (foguete)".
- N-II_(rocket) label "N-II (fusée)".
- N-II_(rocket) label "N-II (rocket)".
- N-II_(rocket) label "N-II (ракета-носитель)".
- N-II_(rocket) label "N-II".
- N-II_(rocket) label "N-IIロケット".
- N-II_(rocket) label "N-II運載火箭".
- N-II_(rocket) sameAs N-II_(fusée).
- N-II_(rocket) sameAs N-II_(roket).
- N-II_(rocket) sameAs N-IIロケット.
- N-II_(rocket) sameAs N-II.
- N-II_(rocket) sameAs N-II_(foguete).
- N-II_(rocket) sameAs m.04jj9ss.
- N-II_(rocket) sameAs Q3130574.
- N-II_(rocket) sameAs Q3130574.
- N-II_(rocket) sameAs N-II_(rocket).
- N-II_(rocket) wasDerivedFrom N-II_(rocket)?oldid=541448503.
- N-II_(rocket) depiction N-II.svg.
- N-II_(rocket) isPrimaryTopicOf N-II_(rocket).