|
gptkbp:instanceOf
|
piston engine
|
|
gptkbp:countryOfOrigin
|
gptkb:United_States
|
|
gptkbp:diameter
|
3.05 m (Titan IV core)
|
|
gptkbp:firstFlight
|
1959
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Titan family of rockets
|
|
gptkbp:launchSite
|
gptkb:Vandenberg_Air_Force_Base
gptkb:Cape_Canaveral_Space_Launch_Complex_40
|
|
gptkbp:length
|
up to 62.8 m (Titan IV)
|
|
gptkbp:manufacturer
|
gptkb:Lockheed_Martin
gptkb:Martin_Marietta
gptkb:Glenn_L._Martin_Company
|
|
gptkbp:notableMission
|
gptkb:Gemini_program
gptkb:Voyager_1
gptkb:Cassini–Huygens
|
|
gptkbp:notableVariant
|
gptkb:Titan_I
gptkb:Titan_II
gptkb:Titan_III
gptkb:Titan_IV
|
|
gptkbp:numberOfLaunches
|
368
|
|
gptkbp:pages
|
https://en.wikipedia.org/wiki/Titan_(rocket_family)
|
|
gptkbp:payloadToGTO
|
up to 5,000 kg (Titan IVB)
|
|
gptkbp:payloadToLEO
|
up to 21,680 kg (Titan IVB)
|
|
gptkbp:propulsion
|
gptkb:water
|
|
gptkbp:retired
|
2005
|
|
gptkbp:status
|
retired
|
|
gptkbp:successor
|
gptkb:Atlas_V
gptkb:Delta_IV
|
|
gptkbp:successRate
|
~90%
|
|
gptkbp:usedBy
|
gptkb:NASA
gptkb:National_Reconnaissance_Office
gptkb:US_Air_Force
|
|
gptkbp:usedFor
|
gptkb:satellite
gptkb:surface-to-air_missile
|
|
gptkbp:bfsParent
|
gptkb:LR91
|
|
gptkbp:bfsLayer
|
7
|