Matches in DBpedia 2015-10 for { <http://dbpedia.org/resource/Delta_IV_Heavy> ?p ?o }
- Delta_IV_Heavy diameter "5.0".
- Delta_IV_Heavy height "72000.0".
- Delta_IV_Heavy mass "733000.0".
- Delta_IV_Heavy mass "733000.0".
- Delta_IV_Heavy abstract "The Delta IV Heavy (Delta 9250H) is an expendable heavy lift launch vehicle, the largest type of the Delta IV family, and the world's highest capacity rocket currently in operation. It was first launched in 2004.The Delta IV Heavy uses two additional Common Booster Cores as liquid rocket boosters instead of the GEM-60 solid rocket motors used by the Delta IV Medium+ versions. At lift off, all three cores operate at full thrust, and 44 seconds later the center core throttles down to 55% to conserve fuel until booster separation. The boosters burn out at 242 seconds after launch, and are separated as the core booster throttles back up to full thrust. The core burns out 86 seconds later, and the second stage completes the ascent to orbit.The first launch of the Delta IV Heavy in 2004 carried a boilerplate payload, and was a partial failure. Cavitation in the liquid oxygen propellant lines caused shutdown of both boosters 8 seconds early, and the core engine 9 seconds early; this resulted in a lower staging velocity for which the second stage was unable to compensate. The payload was left in a lower than intended orbit. Its first operational payload was the DSP-23 satellite, successfully launched in 2007; it was then used to launch a further five visual and electronic reconnaissance satellites for the National Reconnaissance Office through 2013.In December 2014, the Delta IV Heavy was used to launch an uncrewed test flight of the Orion Multi-Purpose Crew Vehicle, designated EFT-1. After several delays on December 4, the mission was successfully launched at 12:05 UTC on December 5.Capacity of the Delta IV Heavy:Low Earth orbit (LEO), 200 km × 28.7°: 28,790 kg (63,470 lb)Low Earth orbit (ISS), 407 km × 51.6°: 25,980 kg (57,280 lb)Geosynchronous transfer orbit (GTO): 14,220 kg (31,350 lb)Geosynchronous orbit (GEO): 6,750 kg (14,880 lb)Lunar transfer orbit (LTO) 10,000 kg (22,000 lb) / Mars transfer orbit 8,000 kg (17,600 lb)The Heavy's total mass at launch is approximately 733,000 kg (1,616,000 lb).".
- Delta_IV_Heavy countryOrigin United_States.
- Delta_IV_Heavy diameter "5.0".
- Delta_IV_Heavy height "72.0".
- Delta_IV_Heavy launchSite Cape_Canaveral_Air_Force_Station.
- Delta_IV_Heavy launchSite Cape_Canaveral_Air_Force_Station_Space_Launch_Complex_37.
- Delta_IV_Heavy launchSite Vandenberg_AFB_Space_Launch_Complex_6.
- Delta_IV_Heavy maidenFlight "2004-12-21".
- Delta_IV_Heavy manufacturer United_Launch_Alliance.
- Delta_IV_Heavy mass "7.33E8".
- Delta_IV_Heavy partialFailedLaunches "1".
- Delta_IV_Heavy rocketFunction Heavy_lift_launch_vehicle.
- Delta_IV_Heavy rocketStages "2".
- Delta_IV_Heavy status "Active".
- Delta_IV_Heavy successfulLaunches "7".
- Delta_IV_Heavy thumbnail Delta_IV_launch_2013-08-28.jpg?width=300.
- Delta_IV_Heavy totalLaunches "8".
- Delta_IV_Heavy wikiPageExternalLink .VHxsvDHF9Zs.
- Delta_IV_Heavy wikiPageID "14018281".
- Delta_IV_Heavy wikiPageLength "9138".
- Delta_IV_Heavy wikiPageOutDegree "54".
- Delta_IV_Heavy wikiPageRevisionID "673254501".
- Delta_IV_Heavy wikiPageWikiLink Angara_(rocket_family).
- Delta_IV_Heavy wikiPageWikiLink Ariane_5.
- Delta_IV_Heavy wikiPageWikiLink Atlas_V.
- Delta_IV_Heavy wikiPageWikiLink Boilerplate_(spaceflight).
- Delta_IV_Heavy wikiPageWikiLink Cape_Canaveral_Air_Force_Station.
- Delta_IV_Heavy wikiPageWikiLink Cape_Canaveral_Air_Force_Station_Space_Launch_Complex_37.
- Delta_IV_Heavy wikiPageWikiLink Category:Delta_(rocket_family).
- Delta_IV_Heavy wikiPageWikiLink Cavitation.
- Delta_IV_Heavy wikiPageWikiLink Common_Booster_Core.
- Delta_IV_Heavy wikiPageWikiLink Defense_Support_Program.
- Delta_IV_Heavy wikiPageWikiLink Delta_Cryogenic_Second_Stage.
- Delta_IV_Heavy wikiPageWikiLink Delta_IV.
- Delta_IV_Heavy wikiPageWikiLink Evolved_Expendable_Launch_Vehicle.
- Delta_IV_Heavy wikiPageWikiLink Exploration_Flight_Test_1.
- Delta_IV_Heavy wikiPageWikiLink Falcon_Heavy.
- Delta_IV_Heavy wikiPageWikiLink Geostationary_transfer_orbit.
- Delta_IV_Heavy wikiPageWikiLink Geosynchronous_orbit.
- Delta_IV_Heavy wikiPageWikiLink Geosynchronous_transfer_orbit.
- Delta_IV_Heavy wikiPageWikiLink Graphite-Epoxy_Motor.
- Delta_IV_Heavy wikiPageWikiLink Heavy_lift_launch_vehicle.
- Delta_IV_Heavy wikiPageWikiLink Hohmann_transfer_orbit.
- Delta_IV_Heavy wikiPageWikiLink LH2.
- Delta_IV_Heavy wikiPageWikiLink LOX.
- Delta_IV_Heavy wikiPageWikiLink Liquid_hydrogen.
- Delta_IV_Heavy wikiPageWikiLink Liquid_oxygen.
- Delta_IV_Heavy wikiPageWikiLink Liquid_rocket_booster.
- Delta_IV_Heavy wikiPageWikiLink Long_March_5.
- Delta_IV_Heavy wikiPageWikiLink Low_Earth_orbit.
- Delta_IV_Heavy wikiPageWikiLink Lunar_transfer_orbit.
- Delta_IV_Heavy wikiPageWikiLink Mars_transfer_orbit.
- Delta_IV_Heavy wikiPageWikiLink National_Reconnaissance_Office.
- Delta_IV_Heavy wikiPageWikiLink Orion_(spacecraft).
- Delta_IV_Heavy wikiPageWikiLink Orion_Multi-Purpose_Crew_Vehicle.
- Delta_IV_Heavy wikiPageWikiLink Proton-M.
- Delta_IV_Heavy wikiPageWikiLink RL10.
- Delta_IV_Heavy wikiPageWikiLink RS-68.
- Delta_IV_Heavy wikiPageWikiLink RS-68A.
- Delta_IV_Heavy wikiPageWikiLink Reconnaissance_satellite.
- Delta_IV_Heavy wikiPageWikiLink Reconnaissance_satellites.
- Delta_IV_Heavy wikiPageWikiLink SLC-37B.
- Delta_IV_Heavy wikiPageWikiLink SLC-6.
- Delta_IV_Heavy wikiPageWikiLink Sea_level.
- Delta_IV_Heavy wikiPageWikiLink Solid-fuel_rocket.
- Delta_IV_Heavy wikiPageWikiLink Solid_rocket_motor.
- Delta_IV_Heavy wikiPageWikiLink Space_Launch_System.
- Delta_IV_Heavy wikiPageWikiLink Titan_IV.
- Delta_IV_Heavy wikiPageWikiLink Trans-Mars_injection.
- Delta_IV_Heavy wikiPageWikiLink United_Launch_Alliance.
- Delta_IV_Heavy wikiPageWikiLink United_States.
- Delta_IV_Heavy wikiPageWikiLink Vacuum.
- Delta_IV_Heavy wikiPageWikiLink Vandenberg_AFB_Space_Launch_Complex_6.
- Delta_IV_Heavy wikiPageWikiLink Vandenberg_Air_Force_Base.
- Delta_IV_Heavy wikiPageWikiLinkText "Delta IV Heavy".
- Delta_IV_Heavy wikiPageWikiLinkText "Delta IV-H".
- Delta_IV_Heavy caption "Delta IV Heavy launches from Vandenberg AFB".
- Delta_IV_Heavy countryOrigin United_States.
- Delta_IV_Heavy cpl "3.75E8".
- Delta_IV_Heavy cplYear "2014".
- Delta_IV_Heavy family Delta_IV.
- Delta_IV_Heavy first "2004-12-21".
- Delta_IV_Heavy function "Orbital heavy lift launch vehicle".
- Delta_IV_Heavy hasPhotoCollection Delta_IV_Heavy.
- Delta_IV_Heavy launches "8".
- Delta_IV_Heavy manufacturer United_Launch_Alliance.
- Delta_IV_Heavy name "Delta IV Heavy".
- Delta_IV_Heavy partial "1".
- Delta_IV_Heavy sites Cape_Canaveral_Air_Force_Station.
- Delta_IV_Heavy sites Cape_Canaveral_Air_Force_Station_Space_Launch_Complex_37.
- Delta_IV_Heavy sites SLC-37B.
- Delta_IV_Heavy sites "SLC-6 Vandenberg AFB".
- Delta_IV_Heavy stages "2".
- Delta_IV_Heavy status "Active".
- Delta_IV_Heavy success "7".
- Delta_IV_Heavy wikiPageUsesTemplate Template:Convert.