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Subject Item

dbpedia:Atlas_II

rdfs:comment

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.

foaf:name

Atlas II

foaf:depiction

n7:jpeg

dbpedia-owl:countryOrigin

dbpedia:United_States

dbpedia-owl:diameter

3.04

dbpedia-owl:finalFlight

2004-08-31Z 1998-03-16Z 2002-12-05Z

dbpedia-owl:height

47.54

dbpedia-owl:launchSite

dbpedia:Vandenberg_AFB_Space_Launch_Complex_3 dbpedia:Spaceport_Florida_Launch_Complex_36 dbpedia:Cape_Canaveral_Air_Force_Station

dbpedia-owl:lowerEarthOrbitPayload

6.58e+06

dbpedia-owl:maidenFlight

1991-12-07Z 1993-12-16Z 1992-06-10Z

dbpedia-owl:manufacturer

dbpedia:Lockheed_Martin

dbpedia-owl:mass

2.043e+08

dbpedia-owl:rocketFunction

dbpedia:Launch_vehicle

dbpedia-owl:rocketStages

4

dbpedia-owl:status

Retired

dbpedia-owl:successfulLaunches

10 63

dbpedia-owl:thumbnail

n6:300

dbpedia-owl:totalLaunches

63 10