Matches in DBpedia 2014 for { <http://dbpedia.org/resource/Delta_II> ?p ?o. }
- Delta_II diameter "2.44".
- Delta_II abstract "Delta II is an American space launch system, originally designed and built by McDonnell Douglas. Delta II is part of the Delta rocket family and entered service in 1989. Delta II vehicles included the Delta 6000, the Delta 7000, and two 7000 variants ("Light" and "Heavy").After McDonnell Douglas merged with Boeing in 1997, Delta II rockets were built by Boeing Integrated Defense Systems, until Delta rocket production became the responsibility of United Launch Alliance (ULA) on December 1, 2006. ULA now markets Delta II to U.S. government customers, and Boeing Launch Services (BLS) markets Delta II to commercial companies.".
- Delta_II countryOrigin United_States.
- Delta_II diameter "2.44".
- Delta_II failedLaunches "1".
- Delta_II finalFlight "1992-07-24".
- Delta_II finalFlight "2011-09-10".
- Delta_II launchSite Cape_Canaveral_Air_Force_Station.
- Delta_II launchSite Vandenberg_Air_Force_Base.
- Delta_II maidenFlight "1989-02-14".
- Delta_II maidenFlight "1990-11-26".
- Delta_II maidenFlight "2003-07-08".
- Delta_II manufacturer United_Launch_Alliance.
- Delta_II partialFailedLaunches "1".
- Delta_II rocketFunction Launch_vehicle.
- Delta_II rocketStages "2".
- Delta_II rocketStages "3".
- Delta_II status "Active".
- Delta_II successfulLaunches "149".
- Delta_II successfulLaunches "6000".
- Delta_II successfulLaunches "7000".
- Delta_II thumbnail Delta_II_Dawn_liftoff_1.jpg?width=300.
- Delta_II totalLaunches "151".
- Delta_II totalLaunches "6000".
- Delta_II totalLaunches "7000".
- Delta_II wikiPageExternalLink delta.
- Delta_II wikiPageExternalLink delta.htm.
- Delta_II wikiPageExternalLink delta2.htm.
- Delta_II wikiPageID "421565".
- Delta_II wikiPageRevisionID "588617420".
- Delta_II alt2AltBoosterthrust "141250".
- Delta_II alt2Boosterengines "1".
- Delta_II alt2Boosterfuel Solid-fuel_rocket.
- Delta_II alt2Boostername Graphite-Epoxy_Motor.
- Delta_II alt2Boosters "9".
- Delta_II alt2Boostersi "278.0".
- Delta_II alt2Boostersthrust "628.3 kN".
- Delta_II alt2Boostertime "75.0".
- Delta_II alt2Diff "7000".
- Delta_II altAltBoosterthrust "110800".
- Delta_II altBoosterengines "1".
- Delta_II altBoosterfuel Solid-fuel_rocket.
- Delta_II altBoostername Graphite-Epoxy_Motor.
- Delta_II altBoosters "34".
- Delta_II altBoostersi "274.0".
- Delta_II altBoostersthrust "492.9 kN".
- Delta_II altBoosterthrust "107530".
- Delta_II altBoostertime "64.0".
- Delta_II altDiff "7000".
- Delta_II altStage1thrust "237000".
- Delta_II altStage2thrust "9800".
- Delta_II altStage3thrust "14837".
- Delta_II boosterengines "1".
- Delta_II boosterfuel Solid-fuel_rocket.
- Delta_II boostername Castor_(rocket_stage).
- Delta_II boosters "9".
- Delta_II boostersi "266.0".
- Delta_II boosterthrust "478.3 kN".
- Delta_II boostertime "56.0".
- Delta_II caption "A Delta II rocket launches from Cape Canaveral carrying the Dawn spacecraft.".
- Delta_II countryOrigin United_States.
- Delta_II cplYear "1987".
- Delta_II diameter "2.44 m".
- Delta_II diff "6000".
- Delta_II fail "1".
- Delta_II first "--02-14".
- Delta_II first "--07-08".
- Delta_II first "--11-26".
- Delta_II function Launch_vehicle.
- Delta_II hasPhotoCollection Delta_II.
- Delta_II height "2340.0".
- Delta_II last "--07-24".
- Delta_II last "--09-10".
- Delta_II launches "151".
- Delta_II launches "Delta 6000: 17".
- Delta_II launches "Delta 7000: 128".
- Delta_II launches "Delta 7000H: 6".
- Delta_II manufacturer "United Launch Alliance".
- Delta_II mass "151700".
- Delta_II name "Delta II".
- Delta_II partial "1".
- Delta_II sites Cape_Canaveral_Air_Force_Station.
- Delta_II sites Cape_Canaveral_Air_Force_Station_Space_Launch_Complex_17.
- Delta_II sites Vandenberg_AFB_Space_Launch_Complex_2.
- Delta_II sites Vandenberg_Air_Force_Base.
- Delta_II stage1engines "1".
- Delta_II stage1fuel Liquid_oxygen.
- Delta_II stage1fuel RP-1.
- Delta_II stage1name "Thor/Delta XLT".
- Delta_II stage1si "302.0".
- Delta_II stage1thrust "1,054.2 kN".
- Delta_II stage1time "265.0".
- Delta_II stage2engines "1".
- Delta_II stage2fuel Aerozine_50.
- Delta_II stage2fuel Dinitrogen_tetroxide.
- Delta_II stage2name "Delta K".
- Delta_II stage2si "319.0".
- Delta_II stage2thrust "43.6 kN".
- Delta_II stage2time "431.0".
- Delta_II stage3engines "1".