Matches in DBpedia 2015-10 for { <http://dbpedia.org/resource/Delta_5000> ?p ?o }
- Delta_5000 abstract "The Delta 5000 series was an American expendable launch system which was used to conduct an orbital launch in 1989. It was a member of the Delta family of rockets. Although several variants were put forward, only the Delta 5920 was launched. The designation used a four digit numerical code to store information on the configuration of the rocket. It was built from a combination of spare parts left over from earlier Delta rockets, which were being retired, and parts from the Delta II 6000-series, which was just entering service.The first stage was the RS-27 powered Extended Long Tank Thor, flown on several earlier Delta rockets. Nine Castor-4A solid rocket boosters were attached to increase thrust at lift-off, replacing the less powerful Castor-4 boosters used on the 3000 series. The Delta-K was used as a second stage. In the configuration that was launched, no third stage was flown.The Delta 5000 was launched just once, from Space Launch Complex 2W at the Vandenberg Air Force Base. Launch occurred at 14:34 on 18 November 1989. It was successful, and placed the Cosmic Background Explorer spacecraft into low Earth orbit.".
- Delta_5000 countryOrigin United_States.
- Delta_5000 launchSite Vandenberg_Air_Force_Base.
- Delta_5000 rocketFunction Expendable_launch_system.
- Delta_5000 status "Retired".
- Delta_5000 successfulLaunches "1".
- Delta_5000 thumbnail COBELaunch.jpg?width=300.
- Delta_5000 totalLaunches "1".
- Delta_5000 wikiPageID "21552740".
- Delta_5000 wikiPageLength "2771".
- Delta_5000 wikiPageOutDegree "34".
- Delta_5000 wikiPageRevisionID "543150933".
- Delta_5000 wikiPageWikiLink AJ-10.
- Delta_5000 wikiPageWikiLink AJ10.
- Delta_5000 wikiPageWikiLink Aerozine.
- Delta_5000 wikiPageWikiLink Aerozine_50.
- Delta_5000 wikiPageWikiLink Castor-4.
- Delta_5000 wikiPageWikiLink Castor-4A.
- Delta_5000 wikiPageWikiLink Castor_(rocket_stage).
- Delta_5000 wikiPageWikiLink Castor_4A.
- Delta_5000 wikiPageWikiLink Category:Delta_(rocket_family).
- Delta_5000 wikiPageWikiLink Cosmic_Background_Explorer.
- Delta_5000 wikiPageWikiLink Delta-K.
- Delta_5000 wikiPageWikiLink Delta_(rocket_family).
- Delta_5000 wikiPageWikiLink Delta_II.
- Delta_5000 wikiPageWikiLink Dinitrogen_tetroxide.
- Delta_5000 wikiPageWikiLink Expendable_launch_system.
- Delta_5000 wikiPageWikiLink Extended_Long_Tank_Thor.
- Delta_5000 wikiPageWikiLink LOX.
- Delta_5000 wikiPageWikiLink Liquid_oxygen.
- Delta_5000 wikiPageWikiLink Low_Earth_orbit.
- Delta_5000 wikiPageWikiLink Newton_(unit).
- Delta_5000 wikiPageWikiLink Orbit.
- Delta_5000 wikiPageWikiLink RP-1.
- Delta_5000 wikiPageWikiLink RS-27.
- Delta_5000 wikiPageWikiLink Solid-fuel_rocket.
- Delta_5000 wikiPageWikiLink Solid_rocket.
- Delta_5000 wikiPageWikiLink Solid_rocket_booster.
- Delta_5000 wikiPageWikiLink United_States.
- Delta_5000 wikiPageWikiLink Vandenberg_AFB_Space_Launch_Complex_2.
- Delta_5000 wikiPageWikiLink Vandenberg_Air_Force_Base.
- Delta_5000 wikiPageWikiLinkText "Delta 5000".
- Delta_5000 wikiPageWikiLinkText "Delta 5920".
- Delta_5000 wikiPageWikiLinkText "Delta 5920-8".
- Delta_5000 boosterengines "1".
- Delta_5000 boosterfuel Solid-fuel_rocket.
- Delta_5000 boosterfuel Solid_rocket.
- Delta_5000 boostername Castor_(rocket_stage).
- Delta_5000 boostername Castor_4A.
- Delta_5000 boosters "9".
- Delta_5000 boostersi "266.0".
- Delta_5000 boosterthrust "478.3 kN".
- Delta_5000 boostertime "56.0".
- Delta_5000 caption "Launch of the Delta 5920 with COBE".
- Delta_5000 function Expendable_launch_system.
- Delta_5000 hasPhotoCollection Delta_5000.
- Delta_5000 launches "1".
- Delta_5000 name "Delta 5000 series".
- Delta_5000 only "1989-11-18".
- Delta_5000 sites Vandenberg_AFB_Space_Launch_Complex_2.
- Delta_5000 sites Vandenberg_Air_Force_Base.
- Delta_5000 stage1engines "1".
- Delta_5000 stage1fuel LOX.
- Delta_5000 stage1fuel Liquid_oxygen.
- Delta_5000 stage1fuel RP-1.
- Delta_5000 stage1name Extended_Long_Tank_Thor.
- Delta_5000 stage1si "302.0".
- Delta_5000 stage1thrust "1,054.2 kN".
- Delta_5000 stage1time "265.0".
- Delta_5000 stage2engines "1".
- Delta_5000 stage2fuel Aerozine.
- Delta_5000 stage2fuel Aerozine_50.
- Delta_5000 stage2fuel Dinitrogen_tetroxide.
- Delta_5000 stage2name Delta-K.
- Delta_5000 stage2si "319.0".
- Delta_5000 stage2thrust "43.6 kN".
- Delta_5000 stage2time "431.0".
- Delta_5000 status "Retired".
- Delta_5000 success "1".
- Delta_5000 wikiPageUsesTemplate Template:Cite_web.
- Delta_5000 wikiPageUsesTemplate Template:Expendable_launch_systems.
- Delta_5000 wikiPageUsesTemplate Template:Infobox_Rocket.
- Delta_5000 wikiPageUsesTemplate Template:Refbegin.
- Delta_5000 wikiPageUsesTemplate Template:Refend.
- Delta_5000 wikiPageUsesTemplate Template:Rocket-stub.
- Delta_5000 wikiPageUsesTemplate Template:Thor_and_Delta_rockets.
- Delta_5000 wikiPageUsesTemplate Template:US_launch_systems.
- Delta_5000 subject Category:Delta_(rocket_family).
- Delta_5000 hypernym System.
- Delta_5000 type MeanOfTransportation.
- Delta_5000 type Rocket.
- Delta_5000 type Vehicle.
- Delta_5000 type DesignedArtifact.
- Delta_5000 type Thing.
- Delta_5000 type Q41291.
- Delta_5000 comment "The Delta 5000 series was an American expendable launch system which was used to conduct an orbital launch in 1989. It was a member of the Delta family of rockets. Although several variants were put forward, only the Delta 5920 was launched. The designation used a four digit numerical code to store information on the configuration of the rocket.".
- Delta_5000 label "Delta 5000".
- Delta_5000 sameAs Delta_5000.
- Delta_5000 sameAs דלתא_5000.
- Delta_5000 sameAs Delta_5000.