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Atlas V 541
URI:
https://gptkb.org/entity/Atlas_V_541
GPTKB entity
Statements (32)
Predicate
Object
gptkbp:instanceOf
launch vehicle configuration
gptkbp:configurationCode
541
gptkbp:coreStage
gptkb:Common_Core_Booster
gptkbp:countryOfOrigin
gptkb:United_States
gptkbp:describes
Atlas V 541 is a configuration of the Atlas V expendable launch system with a 5-meter fairing, 4 solid rocket boosters, and 1 Centaur upper stage engine.
gptkbp:engineType
gptkb:RD-180_(first_stage)
gptkb:RL10_(second_stage)
gptkbp:firstFlight
2012-08-05
https://www.w3.org/2000/01/rdf-schema#label
Atlas V 541
gptkbp:launchSite
gptkb:Cape_Canaveral_Space_Launch_Complex_41
gptkb:Vandenberg_Space_Launch_Complex_3E
gptkbp:manufacturer
gptkb:United_Launch_Alliance
gptkbp:notableMission
gptkb:Mars_Science_Laboratory_(Curiosity_rover)
gptkb:GOES-R
gptkbp:numberOfSolidBoosters
4
gptkbp:numberOfStages
gptkb:Dragon
2
gptkbp:partOf
gptkb:Atlas_V_family
gptkbp:payloadFairingDiameter
5 meters
gptkbp:payloadToGTO
8,290 kg
gptkbp:payloadToLEO
18,810 kg
gptkbp:propulsion
LH2/LOX (second stage)
RP-1/LOX (first stage)
gptkbp:status
active
gptkbp:bfsParent
gptkb:Mars_2020
gptkb:Curiosity_Rover
gptkb:Curiosity_rover
gptkb:Mars_2020_Perseverance_Rover
gptkb:Mars_Science_Laboratory
gptkb:Perseverance_Rover
gptkb:Perseverance_rover
gptkbp:bfsLayer
5