Statements (35)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:aircraft
gptkb:rocket |
| gptkbp:bfsLayer |
4
|
| gptkbp:bfsParent |
gptkb:JAXA
gptkb:Japanese_Aerospace_Exploration_Agency gptkb:Japanese_Aerospace_Exploration_Agency_(JAXA) gptkb:Japan_Aerospace_Exploration_Agency_(JAXA) |
| gptkbp:diameter |
4 meters
|
| gptkbp:first_flight |
gptkb:30
2004-02-20 2004-08-29 |
| gptkbp:height |
53 meters
|
| https://www.w3.org/2000/01/rdf-schema#label |
H-IIA 242
|
| gptkbp:launch_date |
2014-12-03
|
| gptkbp:launch_site |
gptkb:Tanegashima_Space_Center
|
| gptkbp:launch_vehicle |
gptkb:H-IIA
gptkb:H-IIA_202 |
| gptkbp:manufacturer |
gptkb:Mitsubishi_Heavy_Industries
|
| gptkbp:mass |
288,000 kg
|
| gptkbp:mission |
gptkb:spacecraft
successful |
| gptkbp:mission_duration |
varied by payload
|
| gptkbp:number_of_stages |
2
LE-7 A engine H M7 A engine |
| gptkbp:operator |
gptkb:Mitsubishi_Heavy_Industries
|
| gptkbp:seating_capacity |
1,500 kg
10,000 kg 4,000 kg 4,000 kg to geostationary transfer orbit H-IIA 242 payload |
| gptkbp:strategic_importance |
gptkb:0
|
| gptkbp:succeeded_by |
gptkb:10
gptkb:theorem 90% |