Titan I first stage

GPTKB entity

Predicate	Object
gptkbp:instance_of	gptkb:rocket
gptkbp:bfsLayer	5
gptkbp:bfsParent	gptkb:Titan_I
gptkbp:check_in_time	150 seconds
gptkbp:controls	inertial guidance system
gptkbp:cooling_system	regenerative cooling
gptkbp:debut_year	gptkb:1962
gptkbp:decommissioned	gptkb:1965
gptkbp:design	gptkb:weapon
gptkbp:developer	1955-1962
gptkbp:diameter	3.05 meters
gptkbp:engine	gptkb:Rocketdyne two engines
gptkbp:engine_type	gptkb:rocket L R87
gptkbp:first_flight	gptkb:1962 gptkb:1965 gptkb:4
gptkbp:fuel_capacity	2,000 kg/min
gptkbp:fuel_type	kerosene
gptkbp:guidance_system	inertial guidance
gptkbp:has_ability	gptkb:1962
gptkbp:has_programs	gptkb:Titan_I_program
gptkbp:height	30.5 meters
https://www.w3.org/2000/01/rdf-schema#label	Titan I first stage
gptkbp:inspiration	gptkb:Monarch
gptkbp:launch_date	gptkb:1965
gptkbp:launch_site	gptkb:Cape_Canaveral_Air_Force_Station gptkb:railway_station
gptkbp:launch_vehicle	gptkb:Titan_I gptkb:Titan_family gptkb:CEO
gptkbp:launched	gptkb:12 vertical
gptkbp:manufacturer	gptkb:Martin_Company
gptkbp:mass	136,000 kg
gptkbp:metabolism	3,000 kg/min
gptkbp:mission	gptkb:military_unit
gptkbp:number_built	gptkb:12
gptkbp:number_of_stages	gptkb:first_stage after 150 seconds
gptkbp:operational_area	gptkb:aircraft 1962-1965
gptkbp:operational_status	gptkb:1965 retired
gptkbp:propulsion	1.1 RP-1 and Liquid Oxygen 150,000 lbf 150,000 pounds-force
gptkbp:restoration	gptkb:none
gptkbp:role	gptkb:rocket
gptkbp:seating_capacity	3,000 kg to LEO
gptkbp:social_structure	liquid oxygen
gptkbp:successor	gptkb:Titan_II
gptkbp:used_in	gptkb:Titan_I