Atlas V 541

URI: https://gptkb.org/entity/Atlas_V_541

GPTKB entity

Predicate	Object
gptkbp:instanceOf	gptkb: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
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:Curiosity_Rover gptkb:Mars_2020_Perseverance_Rover gptkb:Mars_Science_Laboratory gptkb:Perseverance_Rover
gptkbp:bfsLayer	5
https://www.w3.org/2000/01/rdf-schema#label	Atlas V 541