Matches in DBpedia 2014 for { <http://dbpedia.org/resource/Atlas_II> ?p ?o. }
- Atlas_II diameter "3.04".
- Atlas_II height "47540.0".
- Atlas_II mass "204300.0".
- Atlas_II lowerEarthOrbitPayload "6580.0".
- Atlas_II mass "204300.0".
- Atlas_II abstract "Atlas II was a member of the Atlas family of launch vehicles, which evolved from the successful Atlas missile program of the 1950s. Atlas II was the last Atlas to use a three engine, "stage-and-a-half" design: two of its three engines were jettisoned during ascent, but its fuel tanks and other structural elements were retained. It was designed to launch payloads into low earth orbit, geosynchronous transfer orbit or geosynchronous orbit. Sixty-three launches of the Atlas II, IIA and IIAS models were carried out between 1991 and 2004. (The larger Atlas III was used between 2000 and 2005, and the Atlas V is still in use.)".
- Atlas_II countryOrigin United_States.
- Atlas_II diameter "3.04".
- Atlas_II finalFlight "1998-03-16".
- Atlas_II finalFlight "2002-12-05".
- Atlas_II finalFlight "2004-08-31".
- Atlas_II height "47.54".
- Atlas_II launchSite Cape_Canaveral_Air_Force_Station.
- Atlas_II launchSite Spaceport_Florida_Launch_Complex_36.
- Atlas_II launchSite Vandenberg_AFB_Space_Launch_Complex_3.
- Atlas_II lowerEarthOrbitPayload "6580000.0".
- Atlas_II maidenFlight "1991-12-07".
- Atlas_II maidenFlight "1992-06-10".
- Atlas_II maidenFlight "1993-12-16".
- Atlas_II manufacturer Lockheed_Martin.
- Atlas_II mass "2.043E8".
- Atlas_II rocketFunction Launch_vehicle.
- Atlas_II rocketStages "4".
- Atlas_II status "Retired".
- Atlas_II successfulLaunches "10".
- Atlas_II successfulLaunches "63".
- Atlas_II thumbnail DF-SC-99-00074_cropped_and_rotated.jpeg?width=300.
- Atlas_II totalLaunches "10".
- Atlas_II totalLaunches "63".
- Atlas_II wikiPageExternalLink launch_composite.html.
- Atlas_II wikiPageExternalLink factsheet.asp?fsID=80.
- Atlas_II wikiPageExternalLink atlas2as.htm.
- Atlas_II wikiPageID "848881".
- Atlas_II wikiPageRevisionID "572734479".
- Atlas_II altAltBoosterthrust "470680".
- Atlas_II altBoosterengines "2".
- Atlas_II altBoosterfuel Liquid_oxygen.
- Atlas_II altBoosterfuel RP-1.
- Atlas_II altBoostername MA-5_(rocket_stage).
- Atlas_II altBoosters "1".
- Atlas_II altBoostersi "299.0".
- Atlas_II altBoostersthrust "2,093.3 kN".
- Atlas_II altBoosterthrust "107530".
- Atlas_II altBoostertime "172.0".
- Atlas_II altDiameter "10.0".
- Atlas_II altDiff "all".
- Atlas_II altHeight "156.0".
- Atlas_II altMass "414000.0".
- Atlas_II altStage1thrust "86844".
- Atlas_II altStage2thrust "41592".
- Atlas_II altStage3thrust "220".
- Atlas_II boosterengines "1".
- Atlas_II boosterfuel Solid-fuel_rocket.
- Atlas_II boostername "Castor 4A".
- Atlas_II boosters "4".
- Atlas_II boostersi "266.0".
- Atlas_II boosterthrust "478.3 kN".
- Atlas_II boostertime "56.0".
- Atlas_II caption "Launch of an Atlas II rocket".
- Atlas_II countryOrigin United_States.
- Atlas_II diameter "3.04 m".
- Atlas_II diff "Atlas IIAS".
- Atlas_II family Atlas_(rocket_family).
- Atlas_II first "--06-10".
- Atlas_II first "--12-07".
- Atlas_II first "--12-16".
- Atlas_II function "Medium expendable Launch vehicle".
- Atlas_II hasPhotoCollection Atlas_II.
- Atlas_II height "47.54 m".
- Atlas_II imsize "270".
- Atlas_II last "--03-16".
- Atlas_II last "--08-31".
- Atlas_II last "--12-05".
- Atlas_II launches "63".
- Atlas_II leoPayload "6580.0".
- Atlas_II manufacturer Lockheed_Martin.
- Atlas_II mass "204300.0".
- Atlas_II name "Atlas II".
- Atlas_II payload "2810.0".
- Atlas_II payloadLocation Geostationary_transfer_orbit.
- Atlas_II payloads Solar_and_Heliospheric_Observatory.
- Atlas_II payloads Tracking_and_data_relay_satellite.
- Atlas_II sites Cape_Canaveral_Air_Force_Station.
- Atlas_II sites Spaceport_Florida_Launch_Complex_36.
- Atlas_II sites Vandenberg_AFB_Space_Launch_Complex_3.
- Atlas_II sites Vandenberg_Air_Force_Base.
- Atlas_II stage1engines "1".
- Atlas_II stage1fuel Liquid_oxygen.
- Atlas_II stage1fuel RP-1.
- Atlas_II stage1si "316.0".
- Atlas_II stage1thrust "386 kN".
- Atlas_II stage1time "283.0".
- Atlas_II stage2engines "2".
- Atlas_II stage2fuel Liquid_hydrogen.
- Atlas_II stage2fuel Liquid_oxygen.
- Atlas_II stage2name Centaur.
- Atlas_II stage2si "449.0".
- Atlas_II stage2thrust "147 kN".
- Atlas_II stage2time "392.0".
- Atlas_II stage3engines "1".