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Subject Item
dbpedia:Atlas_LV-3B
rdfs:comment
The Atlas LV-3B, Atlas D Mercury Launch Vehicle or Mercury-Atlas Launch Vehicle, was a man-rated expendable launch system used as part of the United States Project Mercury to send astronauts into low Earth orbit. It was derived from the SM-65D Atlas missile, and was a member of the Atlas family of rockets.The Atlas D missile was the natural choice for Project Mercury since it was the only launch vehicle in the US arsenal that could put the spacecraft into orbit.
foaf:name
Atlas LV-3B
foaf:depiction
n6:jpg
dbpedia-owl:countryOrigin
dbpedia:United_States
dbpedia-owl:diameter
3.048
dbpedia-owl:failedLaunches
2
dbpedia-owl:finalFlight
1963-05-15Z
dbpedia-owl:height
28.7426
dbpedia-owl:launchSite
dbpedia:Cape_Canaveral_Air_Force_Station
dbpedia-owl:lowerEarthOrbitPayload
1.36e+06
dbpedia-owl:maidenFlight
1960-07-29Z
dbpedia-owl:manufacturer
dbpedia:Convair
dbpedia-owl:mass
1.17936e+08
dbpedia-owl:rocketFunction
dbpedia:Human_spaceflight
dbpedia-owl:rocketStages
1
dbpedia-owl:status
Retired
dbpedia-owl:successfulLaunches
7
dbpedia-owl:thumbnail
n4:300
dbpedia-owl:totalLaunches
9