Matches in DBpedia 2015-04 for { <http://dbpedia.org/resource/H-III> ?p ?o }
Showing triples 1 to 63 of
63
with 100 triples per page.
- H-III abstract "H-III (H-X) is an expendable launch system in development in Japan. H-III rockets are liquid-fuelled with solid-fuel strap-on boosters and are planned to be launched from the Tanegashima Space Center in Japan. Mitsubishi and JAXA have been primarily responsible for design, manufacture, and operation of H-III. H-III (without boosters) is able to carry a payload of up to 2,100 kg to GTO, compared with the payload of 4,000-6,000 kg for the H-IIA. Its performance to LEO is 3000 kg to 800km high Sun-synchronous orbit . The first H-III without boosters is planned to launch in 2020, and with boosters in 2021.".
- H-III countryOrigin Japan.
- H-III launchSite Tanegashima_Space_Center.
- H-III launchSite Yoshinobu_Launch_Complex.
- H-III manufacturer Mitsubishi_Heavy_Industries.
- H-III rocketFunction Launch_vehicle.
- H-III rocketStages "2".
- H-III status "In development".
- H-III wikiPageExternalLink .U3K174GSzcx.
- H-III wikiPageID "42749215".
- H-III wikiPageRevisionID "633558329".
- H-III altSso "800.0".
- H-III altStage2thrust "30798".
- H-III boosterengines "1".
- H-III boosterfuel Solid-fuel_rocket.
- H-III boostername "M-34+".
- H-III boosters "0".
- H-III boosterthrust "9,220kN".
- H-III boostertime "114.0".
- H-III countryOrigin Japan.
- H-III diameter "-300.0".
- H-III first "2020".
- H-III function Launch_vehicle.
- H-III height "-3600.0".
- H-III manufacturer Mitsubishi_Heavy_Industries.
- H-III mass "215000".
- H-III name "H-III".
- H-III payload "2100".
- H-III payloadLocation "GTO ⊿V=1500m/s".
- H-III sites Tanegashima_Space_Center.
- H-III sites Yoshinobu_Launch_Complex.
- H-III ssoPayload "3000.0".
- H-III stage1engines "2".
- H-III stage1fuel Liquid_hydrogen.
- H-III stage1fuel Liquid_oxygen.
- H-III stage1thrust "2,900kN".
- H-III stage2engines "1".
- H-III stage2fuel Liquid_hydrogen.
- H-III stage2fuel Liquid_oxygen.
- H-III stage2thrust "137 kN".
- H-III stages "2".
- H-III status "In development".
- H-III subject Category:Mitsubishi_Heavy_Industries_space_launch_vehicles.
- H-III subject Category:Space_launch_vehicles_of_Japan.
- H-III type MeanOfTransportation.
- H-III type Rocket.
- H-III type DesignedArtifact.
- H-III type Thing.
- H-III type Q41291.
- H-III comment "H-III (H-X) is an expendable launch system in development in Japan. H-III rockets are liquid-fuelled with solid-fuel strap-on boosters and are planned to be launched from the Tanegashima Space Center in Japan. Mitsubishi and JAXA have been primarily responsible for design, manufacture, and operation of H-III. H-III (without boosters) is able to carry a payload of up to 2,100 kg to GTO, compared with the payload of 4,000-6,000 kg for the H-IIA.".
- H-III label "H-III".
- H-III label "H-III".
- H-III label "H-III".
- H-III label "H-IIIロケット".
- H-III sameAs H-III.
- H-III sameAs H-IIIロケット.
- H-III sameAs H-III.
- H-III sameAs m.010lrhsf.
- H-III sameAs Q11222053.
- H-III sameAs Q11222053.
- H-III wasDerivedFrom H-III?oldid=633558329.
- H-III isPrimaryTopicOf H-III.
- H-III name "H-III".