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