Statements (26)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:Team_Rocket
|
| gptkbp:country |
gptkb:Japan
|
| gptkbp:debut |
gptkb:H-IIA_296
|
| gptkbp:diameter |
4 meters
|
| gptkbp:first_flight |
2004-08-29
|
| gptkbp:flight_style |
29
|
| gptkbp:height |
53 meters
|
| https://www.w3.org/2000/01/rdf-schema#label |
H-IIA 295
|
| gptkbp:launch_date |
2019-01-18
|
| gptkbp:launch_site |
gptkb:Tanegashima_Space_Center
|
| gptkbp:launch_vehicle |
gptkb:H-IIA
|
| gptkbp:launched |
gptkb:1
|
| gptkbp:manufacturer |
gptkb:Mitsubishi_Heavy_Industries
|
| gptkbp:mission |
Communications satellite deployment
|
| gptkbp:number_of_stages |
gptkb:HM7_A_engine
LE-7 A engine |
| gptkbp:orbital_inclination |
gptkb:geostationary_orbit
|
| gptkbp:payload_capacity |
10,000 kg
4,000 kg 4,000 kg to geostationary transfer orbit |
| gptkbp:previous_launches |
gptkb:H-IIA_294
|
| gptkbp:reliability |
high
|
| gptkbp:success |
gptkb:1
|
| gptkbp:success_rate |
97%
|
| gptkbp:bfsParent |
gptkb:JAXA
|
| gptkbp:bfsLayer |
4
|