Delta II 7925H launch vehicle

GPTKB entity

Predicate	Object
gptkbp:instanceOf	gptkb:satellite
gptkbp:configuration	7925H
gptkbp:countryOfOrigin	gptkb:United_States
gptkbp:diameter	2.44 m
gptkbp:family	gptkb:Delta_II
gptkbp:first_stage	Extra-extended Long Tank Thor
gptkbp:first_stage_engine	gptkb:RS-27A
gptkbp:firstFlight	August 17, 1998
gptkbp:height	39 m
gptkbp:launchSite	gptkb:Cape_Canaveral_SLC-17 gptkb:Vandenberg_SLC-2W
gptkbp:manufacturer	gptkb:Boeing gptkb:McDonnell_Douglas
gptkbp:mass	232,870 kg
gptkbp:notable_launches	gptkb:Phoenix_Mars_Lander gptkb:Mars_Exploration_Rovers gptkb:Mars_Odyssey
gptkbp:number_of_solid_rocket_boosters	9
gptkbp:payload_to_GTO	2,170 kg
gptkbp:payloadToLEO	6,100 kg
gptkbp:second_stage	gptkb:Delta-K
gptkbp:second_stage_engine	Aerojet AJ10-118K
gptkbp:solid_rocket_boosters	gptkb:GEM-46
gptkbp:status	retired
gptkbp:third_stage	gptkb:Star_48B
gptkbp:third_stage_type	gptkb:solid_rocket_motor
gptkbp:bfsParent	gptkb:3_GEM-40_boosters
gptkbp:bfsLayer	8
https://www.w3.org/2000/01/rdf-schema#label	Delta II 7925H launch vehicle