Matches in DBpedia 2014 for { <http://dbpedia.org/resource/GX_(rocket)> ?p ?o. }
Showing items 1 to 90 of
90
with 100 items per page.
- GX_(rocket) diameter "3.3".
- GX_(rocket) height "48000.0".
- GX_(rocket) mass "190500.0".
- GX_(rocket) lowerEarthOrbitPayload "3600.0".
- GX_(rocket) mass "190500.0".
- GX_(rocket) abstract "GX was a design for an expendable launch system intended to compete in the commercial satellite launch sector. The system had developed by Galaxy Express Corporation, a joint venture between IHI Corporation (IHI), the Japan Aerospace Exploration Agency (JAXA), United Launch Alliance (ULA), Lockheed Martin Corporation (LM) and several other Japanese companies.The GX design uses a two stage rocket. The first stage would have been the Atlas Common Core Booster, currently used as the first stage of the Atlas V rocket, which would have been provided by United Launch Alliance. The second stage was to be a newly designed stage produced by IHI, using liquefied natural gas as fuel and liquid oxygen as an oxidizer. The GX would have been the only space vehicle to use that combination of fuel and oxidizer. The Japanese government finally abandoned the GX program in December 2009. Galaxy Express disbanded around March 2010.".
- GX_(rocket) countryOrigin Japan.
- GX_(rocket) countryOrigin United_States.
- GX_(rocket) diameter "3.3".
- GX_(rocket) height "48.0".
- GX_(rocket) launchSite Vandenberg_Air_Force_Base.
- GX_(rocket) lowerEarthOrbitPayload "3600000.0".
- GX_(rocket) manufacturer Galaxy_Express_Corporation.
- GX_(rocket) manufacturer IHI_Corporation.
- GX_(rocket) manufacturer United_Launch_Alliance.
- GX_(rocket) mass "1.905E8".
- GX_(rocket) rocketFunction Launch_vehicle.
- GX_(rocket) rocketStages "2".
- GX_(rocket) status "Cancelled 2010".
- GX_(rocket) wikiPageID "1818086".
- GX_(rocket) wikiPageRevisionID "599877038".
- GX_(rocket) altLeo "4".
- GX_(rocket) altMass "210".
- GX_(rocket) altPayload "2".
- GX_(rocket) altStage1thrust "933406".
- GX_(rocket) caption "GX".
- GX_(rocket) countryOrigin Japan.
- GX_(rocket) countryOrigin United_States.
- GX_(rocket) diameter "3.3m".
- GX_(rocket) function "Medium expendable Launch vehicle".
- GX_(rocket) hasPhotoCollection GX_(rocket).
- GX_(rocket) height "48m".
- GX_(rocket) leoPayload "3600.0".
- GX_(rocket) manufacturer "Galaxy Express".
- GX_(rocket) mass "190500.0".
- GX_(rocket) name "Galaxy Express".
- GX_(rocket) payload "1814.0".
- GX_(rocket) payloadLocation "800".
- GX_(rocket) sites Vandenberg_AFB_Space_Launch_Complex_3.
- GX_(rocket) sites Vandenberg_Air_Force_Base.
- GX_(rocket) stage1engines "1".
- GX_(rocket) stage1fuel Liquid_oxygen.
- GX_(rocket) stage1fuel RP-1.
- GX_(rocket) stage1name Common_Core_Booster.
- GX_(rocket) stage1si "311.0".
- GX_(rocket) stage1thrust "4,152 kN".
- GX_(rocket) stage1time "253.0".
- GX_(rocket) stage2engines "1".
- GX_(rocket) stage2fuel Liquefied_natural_gas.
- GX_(rocket) stage2fuel Liquid_oxygen.
- GX_(rocket) stage2name "GX".
- GX_(rocket) stage2si "323.0".
- GX_(rocket) stage2thrust "118 kN".
- GX_(rocket) stage2time "480.0".
- GX_(rocket) stages "2".
- GX_(rocket) status "Cancelled 2010".
- GX_(rocket) subject Category:Atlas_(rocket_family).
- GX_(rocket) subject Category:Space_launch_vehicles_of_Japan.
- GX_(rocket) type Artifact100021939.
- GX_(rocket) type Conveyance103100490.
- GX_(rocket) type Instrumentality103575240.
- GX_(rocket) type Object100002684.
- GX_(rocket) type PhysicalEntity100001930.
- GX_(rocket) type Rocket104099429.
- GX_(rocket) type SpaceLaunchVehiclesOfJapan.
- GX_(rocket) type Vehicle104524313.
- GX_(rocket) type Whole100003553.
- GX_(rocket) type MeanOfTransportation.
- GX_(rocket) type Rocket.
- GX_(rocket) type RocketEngine.
- GX_(rocket) type DesignedArtifact.
- GX_(rocket) comment "GX was a design for an expendable launch system intended to compete in the commercial satellite launch sector. The system had developed by Galaxy Express Corporation, a joint venture between IHI Corporation (IHI), the Japan Aerospace Exploration Agency (JAXA), United Launch Alliance (ULA), Lockheed Martin Corporation (LM) and several other Japanese companies.The GX design uses a two stage rocket.".
- GX_(rocket) label "GX (foguete)".
- GX_(rocket) label "GX (fusée)".
- GX_(rocket) label "GX (rakieta)".
- GX_(rocket) label "GX (rocket)".
- GX_(rocket) label "GXロケット".
- GX_(rocket) sameAs GX_(fusée).
- GX_(rocket) sameAs GX_(roket).
- GX_(rocket) sameAs GXロケット.
- GX_(rocket) sameAs GX_(로켓).
- GX_(rocket) sameAs GX_(rakieta).
- GX_(rocket) sameAs GX_(foguete).
- GX_(rocket) sameAs m.05zc6h.
- GX_(rocket) sameAs Q1076048.
- GX_(rocket) sameAs Q1076048.
- GX_(rocket) sameAs GX_(rocket).
- GX_(rocket) wasDerivedFrom GX_(rocket)?oldid=599877038.
- GX_(rocket) isPrimaryTopicOf GX_(rocket).
- GX_(rocket) name "Galaxy Express (GX)".