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gptkbp:instanceOf
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gptkb:satellite
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gptkbp:configuration
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4-meter fairing, 2 solid boosters, 1 Centaur engine
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gptkbp:coreStage
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gptkb:Atlas_Common_Core_Booster
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gptkbp:countryOfOrigin
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gptkb:United_States
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gptkbp:diameter
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3.81 meters
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gptkbp:family
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gptkb:Atlas_V
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gptkbp:firstFlight
|
2007-06-15
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|
https://www.w3.org/2000/01/rdf-schema#label
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Atlas V 421
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gptkbp:launchSite
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gptkb:Cape_Canaveral_Space_Launch_Complex_41
gptkb:Vandenberg_Space_Launch_Complex_3E
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gptkbp:length
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58.3 meters
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gptkbp:manufacturer
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gptkb:United_Launch_Alliance
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gptkbp:massToGTO
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5,760 kg
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gptkbp:missionType
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gptkb:RD-180_(first_stage)
gptkb:RL10A-4-2_(second_stage)
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gptkbp:numberOfSolidBoosters
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2
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gptkbp:numberOfStages
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gptkb:Dragon
2
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gptkbp:payloadFairingDiameter
|
4 meters
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gptkbp:payloadToLEO
|
13,620 kg
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gptkbp:propulsion
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LH2/LOX (second stage)
RP-1/LOX (first stage)
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gptkbp:solidBoosterType
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gptkb:Aerojet_Rocketdyne_AJ-60A
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gptkbp:status
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active
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gptkbp:thrust
|
3.8 MN (first stage)
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gptkbp:usedFor
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interplanetary missions
satellite launches
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gptkbp:bfsParent
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gptkb:Magnetospheric_Multiscale_Mission
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gptkbp:bfsLayer
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6
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