|
gptkbp:instanceOf
|
piston engine
|
|
gptkbp:countryOfOrigin
|
gptkb:United_States
|
|
gptkbp:diameter
|
up to 3.05 m
|
|
gptkbp:engineType
|
gptkb:LR-87
gptkb:LR-91
|
|
gptkbp:firstFlight
|
1959
|
|
gptkbp:fuelType
|
gptkb:Aerozine_50
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Titan rocket family
|
|
gptkbp:launchSite
|
gptkb:Vandenberg_Air_Force_Base
gptkb:Cape_Canaveral
|
|
gptkbp:length
|
up to 62.8 m (Titan IV)
|
|
gptkbp:manufacturer
|
gptkb:Lockheed_Martin
gptkb:Martin_Marietta
gptkb:Glenn_L._Martin_Company
|
|
gptkbp:notableFeature
|
first US ICBM with storable propellants
used for both military and civilian space launches
|
|
gptkbp:notableMission
|
gptkb:KH-9_Hexagon_satellites
gptkb:Landsat_satellites
gptkb:Defense_Support_Program_satellites
gptkb:Milstar_satellites
gptkb:Voyager_1
gptkb:Cassini-Huygens
gptkb:Mars_Observer
gptkb:Gemini_missions
gptkb:KH-11_Kennan_satellites
|
|
gptkbp:notableVariant
|
gptkb:Titan_23G
gptkb:Titan_I
gptkb:Titan_II
gptkb:Titan_III
gptkb:Titan_IV
|
|
gptkbp:numberOfLaunches
|
368
|
|
gptkbp:oxidizer
|
gptkb:Nitrogen_tetroxide
|
|
gptkbp:payloadCapacityGTO
|
up to 12,700 kg (Titan IV)
|
|
gptkbp:payloadToLEO
|
up to 23,000 kg (Titan IV)
|
|
gptkbp:propulsion
|
gptkb:water
|
|
gptkbp:replacedBy
|
gptkb:Atlas_V
gptkb:Delta_IV
|
|
gptkbp:retired
|
2005
|
|
gptkbp:status
|
retired
|
|
gptkbp:successRate
|
~90%
|
|
gptkbp:thrust
|
up to 11.5 MN (Titan IV with SRBs)
|
|
gptkbp:usedBy
|
gptkb:NASA
gptkb:National_Reconnaissance_Office
gptkb:US_Air_Force
|
|
gptkbp:usedFor
|
gptkb:ICBM
space launches
launching reconnaissance satellites
military launches
launching Gemini spacecraft
|
|
gptkbp:bfsParent
|
gptkb:Lockheed_Martin_Space
gptkb:Titan_III_rocket
gptkb:Titan_II_rocket
gptkb:Titan_IIIC_launch_vehicle
gptkb:Titan_IV_rocket
gptkb:Titan_III
gptkb:Titan_IV
|
|
gptkbp:bfsLayer
|
6
|