|
gptkbp:instanceOf
|
gptkb:satellite
|
|
gptkbp:configurationVariants
|
401
421
541
431
531
501
521
411
551
511
|
|
gptkbp:countryOfOrigin
|
gptkb:United_States
|
|
gptkbp:diameter
|
3.81 meters
|
|
gptkbp:engine
|
gptkb:RD-180
|
|
gptkbp:family
|
gptkb:Atlas_rocket_family
|
|
gptkbp:firstFlight
|
2002-08-21
|
|
gptkbp:height
|
58.3 meters
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Atlas V rocket
|
|
gptkbp:launchSite
|
gptkb:Cape_Canaveral_Space_Launch_Complex_41
gptkb:Vandenberg_Space_Launch_Complex_3E
|
|
gptkbp:manufacturer
|
gptkb:Lockheed_Martin
gptkb:United_Launch_Alliance
|
|
gptkbp:mass
|
334,500 kg
|
|
gptkbp:notableMission
|
gptkb:Boeing_CST-100_Starliner_OFT-2
gptkb:Landsat_8
gptkb:Mars_2020_(Perseverance_rover)
gptkb:Mars_Science_Laboratory_(Curiosity_rover)
gptkb:Juno
gptkb:New_Horizons
|
|
gptkbp:numberOfLaunches
|
over 90
|
|
gptkbp:numberOfStages
|
gptkb:RL10
2
|
|
gptkbp:payloadToGTO
|
8,900 kg
|
|
gptkbp:payloadToLEO
|
18,850 kg
|
|
gptkbp:propulsion
|
RP-1/LOX
Hydrogen/LOX
|
|
gptkbp:retired
|
2025
|
|
gptkbp:status
|
active
|
|
gptkbp:successor
|
gptkb:Vulcan_Centaur
|
|
gptkbp:successRate
|
over 97%
|
|
gptkbp:usedBy
|
gptkb:NASA
gptkb:US_Department_of_Defense
commercial customers
|
|
gptkbp:usedFor
|
interplanetary missions
launching satellites
crewed missions (Boeing CST-100 Starliner)
|
|
gptkbp:website
|
https://www.ulalaunch.com/rockets/atlas-v
|
|
gptkbp:bfsParent
|
gptkb:Aerojet_Rocketdyne
|
|
gptkbp:bfsLayer
|
5
|