Statements (26)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:rocket
|
| gptkbp:bfsLayer |
4
|
| gptkbp:bfsParent |
gptkb:Tanegashima_Space_Center
|
| gptkbp:diameter |
4 meters
|
| gptkbp:first_flight |
2004-02-20
2014-11-29 |
| gptkbp:height |
53 meters
|
| https://www.w3.org/2000/01/rdf-schema#label |
H-IIA 209 rocket
|
| gptkbp:launch_site |
gptkb:Tanegashima_Space_Center
gptkb:JAXA |
| gptkbp:launch_vehicle |
gptkb:H-IIA
|
| gptkbp:launched |
gptkb:15
|
| gptkbp:manufacturer |
gptkb:Mitsubishi_Heavy_Industries
|
| gptkbp:notable_album |
H-IIA 209 launched the Akasaki satellite
|
| gptkbp:number_of_stages |
gptkb:LE-5_B
gptkb:LE-7_A 2 |
| gptkbp:operational_status |
Retired
|
| gptkbp:origin |
gptkb:Japan
|
| gptkbp:propulsion |
Liquid oxygen and kerosene
|
| gptkbp:reliability |
100%
|
| gptkbp:seating_capacity |
4 meters in diameter
4,000 kg to geostationary transfer orbit |
| gptkbp:setting |
gptkb:H-IIA_202
|
| gptkbp:strategic_importance |
gptkb:0
|
| gptkbp:succeeded_by |
gptkb:15
|