|
gptkbp:instanceOf
|
gptkb:satellite
|
|
gptkbp:configuration
|
triple-core booster
|
|
gptkbp:coreEngines
|
3 RS-68A
|
|
gptkbp:costPerLaunch
|
$350 million (approximate)
|
|
gptkbp:countryOfOrigin
|
gptkb:United_States
|
|
gptkbp:diameter
|
5.1 m
|
|
gptkbp:family
|
gptkb:Delta_IV
|
|
gptkbp:firstFlight
|
2004-12-21
|
|
gptkbp:height
|
72 m
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Boeing Delta IV Heavy
|
|
gptkbp:launched
|
16
|
|
gptkbp:launchSite
|
gptkb:Cape_Canaveral_Space_Launch_Complex_37B
gptkb:Vandenberg_Space_Launch_Complex_6
|
|
gptkbp:manufacturer
|
gptkb:Boeing
gptkb:United_Launch_Alliance
|
|
gptkbp:mass
|
733,000 kg
|
|
gptkbp:notableMission
|
gptkb:Orion_EFT-1
gptkb:NROL-44
gptkb:Parker_Solar_Probe
|
|
gptkbp:numberOfStages
|
gptkb:Common_Booster_Core
gptkb:RL10B-2
2
|
|
gptkbp:operator
|
gptkb:United_Launch_Alliance
|
|
gptkbp:payloadToGTO
|
14,220 kg
|
|
gptkbp:payloadToLEO
|
28,790 kg
|
|
gptkbp:propulsion
|
liquid oxygen
liquid hydrogen
|
|
gptkbp:retired
|
2024-04-09
|
|
gptkbp:status
|
retired
|
|
gptkbp:successor
|
gptkb:Vulcan_Centaur
|
|
gptkbp:usedFor
|
launching heavy payloads to orbit
|
|
gptkbp:website
|
https://www.ulalaunch.com/rockets/delta-iv
|
|
gptkbp:bfsParent
|
gptkb:Boeing
|
|
gptkbp:bfsLayer
|
5
|