Statements (23)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:rocket
|
| gptkbp:bfsLayer |
4
|
| gptkbp:bfsParent |
gptkb:LE-7_A
|
| gptkbp:country |
gptkb:Japan
|
| gptkbp:developer |
$1 billion
|
| gptkbp:diameter |
4 meters
|
| gptkbp:first_flight |
gptkb:1994
|
| gptkbp:height |
47 meters
|
| https://www.w3.org/2000/01/rdf-schema#label |
H-II rocket
|
| gptkbp:is_used_for |
satellite launches
|
| gptkbp:launch_site |
gptkb:Tanegashima_Space_Center
|
| gptkbp:launch_vehicle |
H-II family
|
| gptkbp:launched |
gptkb:15
|
| gptkbp:manufacturer |
gptkb:Mitsubishi_Heavy_Industries
|
| gptkbp:notable_album |
H-II 202
|
| gptkbp:number_of_stages |
gptkb:LE-7_engine
2 LE-5 engine |
| gptkbp:propulsion |
liquid hydrogen and liquid oxygen
|
| gptkbp:reliability |
73.3%
|
| gptkbp:retired |
gptkb:2003
|
| gptkbp:seating_capacity |
10,000 kg
|
| gptkbp:successor |
gptkb:rocket
|