Statements (27)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:diameter |
about 3 meters (Titan II)
|
| gptkbp:firstFlight |
1959
|
| https://www.w3.org/2000/01/rdf-schema#label |
Martin Titan rocket
|
| gptkbp:length |
about 31 meters (Titan II)
|
| gptkbp:manufacturer |
gptkb:Martin_Company
|
| gptkbp:notableVariant |
gptkb:Titan_II
gptkb:Titan_III gptkb:Titan_IV |
| gptkbp:numberOfStages |
2
|
| gptkbp:payloadToLEO |
up to 17,600 kg (Titan IV)
|
| gptkbp:propulsion |
gptkb:water
|
| gptkbp:retired |
2005
|
| gptkbp:status |
retired
|
| gptkbp:successor |
gptkb:Atlas_V
gptkb:Delta_IV |
| gptkbp:usedAs |
gptkb:ICBM
space launch vehicle |
| gptkbp:usedFor |
gptkb:military
gptkb:satellite |
| gptkbp:usedIn |
gptkb:NASA
gptkb:US_Air_Force gptkb:Gemini_program |
| gptkbp:bfsParent |
gptkb:Glenn_L._Martin_Aircraft_Plant
gptkb:Glenn_L._Martin_Company |
| gptkbp:bfsLayer |
5
|