Statements (20)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:rocket
|
| gptkbp:bfsLayer |
5
|
| gptkbp:bfsParent |
gptkb:H-IIA_series
|
| gptkbp:diameter |
4 meters
|
| gptkbp:engine_type |
gptkb:LE-7_A
|
| gptkbp:first_flight |
gptkb:2001
|
| gptkbp:fuel_type |
Liquid hydrogen and kerosene
|
| gptkbp:height |
53 meters
|
| https://www.w3.org/2000/01/rdf-schema#label |
H-IIA 2046
|
| gptkbp:launch_date |
2004-2006
|
| gptkbp:launch_site |
gptkb:Tanegashima_Space_Center
|
| gptkbp:manufacturer |
gptkb:Mitsubishi_Heavy_Industries
|
| gptkbp:notable_album |
H-IIA 202, H-IIA 204, H-IIA 205
|
| gptkbp:number_of_stages |
2
|
| gptkbp:orbital_inclination |
20 degrees
|
| gptkbp:primary_source |
gptkb:spacecraft
|
| gptkbp:propulsion |
1,000 k N
|
| gptkbp:reliability |
high reliability
|
| gptkbp:seating_capacity |
4,000 kg to geostationary transfer orbit
|
| gptkbp:succeeded_by |
multiple successful launches
|