Delta Cryogenic Second Stage

GPTKB entity

Predicate	Object
gptkbp:instance_of	gptkb:Team_Rocket
gptkbp:check_in_time	approximately 10 minutes
gptkbp:configuration	single-engine
gptkbp:debut	gptkb:2019 gptkb:Delta_IV_M+_4,2
gptkbp:design	approximately 15 years
gptkbp:development	1990s
gptkbp:diameter	5.1 meters
gptkbp:engine_type	gptkb:RL10
gptkbp:first_flight	gptkb:2002
gptkbp:function	upper stage propulsion
gptkbp:height	4.1 meters
https://www.w3.org/2000/01/rdf-schema#label	Delta Cryogenic Second Stage
gptkbp:influenced_by	gptkb:Centaur
gptkbp:launch_site	gptkb:Vandenberg_Space_Force_Base gptkb:Cape_Canaveral_Space_Force_Station
gptkbp:launched	satellites
gptkbp:manufacturer	gptkb:NASA
gptkbp:notable_launches	gptkb:James_Webb_Space_Telescope gptkb:NROL-44 gptkb:DMSP-19 gptkb:HST_Servicing_Mission_4 gptkb:Parker_Solar_Probe gptkb:GOES-R gptkb:Landsat_9 gptkb:Mars_2020 gptkb:TESS gptkb:GPS_III-1 WGS-10
gptkbp:number_of_engines	gptkb:1
gptkbp:operated_by	gptkb:United_Launch_Alliance
gptkbp:operational_status	retired
gptkbp:payload_capacity	4,000 kg to GTO
gptkbp:propulsion	liquid oxygen 25,000 lbf liquid hydrogen
gptkbp:related_to	gptkb:Delta_II gptkb:Atlas_V
gptkbp:replaced_by	Centaur upper stage
gptkbp:successor	gptkb:Delta_IV_Heavy
gptkbp:used_for	interplanetary missions
gptkbp:used_in	gptkb:Delta_IV_rocket gptkb:NASA_missions
gptkbp:bfsParent	gptkb:Delta_IV
gptkbp:bfsLayer	4