Statements (16)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:Team_Rocket
|
| gptkbp:diameter |
3.05 meters
|
| gptkbp:engine_type |
gptkb:Team_Rocket
|
| gptkbp:first_flight |
1982-04-05
1966-12-08 |
| gptkbp:height |
34.4 meters
|
| https://www.w3.org/2000/01/rdf-schema#label |
Titan II R
|
| gptkbp:launch_mass |
150,000 kg
|
| gptkbp:manufacturer |
gptkb:Martin_Marietta
|
| gptkbp:number_of_engines |
2
|
| gptkbp:payload_capacity |
3,800 kg
|
| gptkbp:propulsion |
RP-1 and Liquid Oxygen
|
| gptkbp:success_rate |
90%
|
| gptkbp:used_for |
military and civilian satellite launches
|
| gptkbp:bfsParent |
gptkb:Titan_II
|
| gptkbp:bfsLayer |
5
|