Delta Cryogenic Second Stage

URI: https://gptkb.org/entity/Delta_Cryogenic_Second_Stage
GPTKB entity
Statements (45)
Predicate Object
gptkbp:instance_of gptkb:rocket
gptkbp:bfsLayer 4
gptkbp:bfsParent gptkb:Delta_IV
gptkbp:check_in_time approximately 10 minutes
gptkbp:debut_year gptkb:2019
gptkbp:design approximately 15 years
gptkbp:developer 1990s
gptkbp:diameter 5.1 meters
gptkbp:engine gptkb:musical
gptkbp:engine_type R L10
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:dinosaur
gptkbp:is_used_for interplanetary missions
gptkbp:launch_date Delta IVM+ 4,2
gptkbp:launch_site gptkb:Cape_Canaveral_Space_Force_Station
gptkb:software
gptkbp:launched satellites
gptkbp:manufacturer gptkb:NASA
gptkbp:notable_album 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
WGS-10
GPSIII-1
gptkbp:operated_by gptkb:United_Launch_Alliance
gptkbp:operational_status retired
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:seating_capacity 4,000 kg to GTO
gptkbp:setting single-engine
gptkbp:successor gptkb:Delta_IV_Heavy
gptkbp:used_in gptkb:Delta_IV_rocket
gptkb:NASA_missions