Statements (25)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:Team_Rocket
|
| gptkbp:debut |
multiple launches
|
| gptkbp:diameter |
4 meters
|
| gptkbp:engine_type |
gptkb:LE-7_A
|
| gptkbp:first_flight |
gptkb:2004
|
| gptkbp:height |
53 meters
|
| https://www.w3.org/2000/01/rdf-schema#label |
H-IIA 251 rocket
|
| gptkbp:launch_date |
2014-02-22
2004-08-29 |
| gptkbp:launch_event |
over 90%
|
| gptkbp:launch_site |
gptkb:Tanegashima_Space_Center
|
| gptkbp:launch_vehicle |
2
expendable launch system H-II |
| gptkbp:manufacturer |
gptkb:Mitsubishi_Heavy_Industries
|
| gptkbp:mass |
290,000 kg
|
| gptkbp:notable_mission |
gptkb:Akasaki_satellite
|
| gptkbp:number_of_stages |
2
|
| gptkbp:operational_status |
retired
|
| gptkbp:payload_capacity |
10,000 kg
4,000 kg |
| gptkbp:purpose |
gptkb:Space_Launch_System
|
| gptkbp:success_rate |
high
|
| gptkbp:bfsParent |
gptkb:Tanegashima_Space_Center
|
| gptkbp:bfsLayer |
4
|