Titan II

GPTKB entity

Statements (65)

Predicate	Object
gptkbp:instance_of	gptkb:Team_Rocket
gptkbp:configuration	gptkb:Titan_II_GLV gptkb:Titan_II_D gptkb:Titan_II_E gptkb:Titan_II_F gptkb:Titan_II_G gptkb:Titan_II_H gptkb:Titan_II_ICBM gptkb:Titan_II_J gptkb:Titan_II_K gptkb:Titan_II_L gptkb:Titan_II_M gptkb:Titan_II_N gptkb:Titan_II_O gptkb:Titan_II_P gptkb:Titan_II_Q gptkb:Titan_II_R gptkb:Titan_II_S gptkb:Titan_II_T gptkb:Titan_II_U gptkb:Titan_II_V gptkb:Titan_II_W gptkb:Titan_II_X gptkb:Titan_II_Y gptkb:Titan_II_Z
gptkbp:diameter	3.05 meters
gptkbp:engine_type	gptkb:Team_Rocket
gptkbp:first_flight	1962-01-30 1987-04-05
gptkbp:height	34.4 meters 32.5 meters
https://www.w3.org/2000/01/rdf-schema#label	Titan II
gptkbp:launch_mass	150,000 kg
gptkbp:launch_site	gptkb:Cape_Canaveral_Air_Force_Station
gptkbp:manufacturer	gptkb:Martin_Marietta
gptkbp:notable_launches	gptkb:Gemini_12 gptkb:Gemini_3 gptkb:Gemini_4 gptkb:Gemini_5 gptkb:Gemini_6_A gptkb:Gemini_7 gptkb:Gemini_8 gptkb:Gemini_10 gptkb:Gemini_11 gptkb:Gemini_9_A
gptkbp:number_of_engines	2
gptkbp:number_of_stages	gptkb:Titan_II_first_stage gptkb:Titan_II_second_stage
gptkbp:payload_capacity	3,400 kg 9,000 kg to LEO
gptkbp:propulsion	RP-1 and liquid oxygen
gptkbp:retirement_year	gptkb:1987
gptkbp:role	military and civilian launch vehicle
gptkbp:success_rate	95%
gptkbp:successor	gptkb:Titan_III
gptkbp:used_in	gptkb:Gemini_program
gptkbp:bfsParent	gptkb:Thiokol gptkb:KSC_Launch_Complex_75 gptkb:KSC_Launch_Complex_96 gptkb:Gemini_4 gptkb:Gemini_program gptkb:Gemini_Program gptkb:Landsat_series gptkb:Gemini_spacecraft
gptkbp:bfsLayer	4