Statements (31)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:rocket
|
| gptkbp:bfsLayer |
4
|
| gptkbp:bfsParent |
gptkb:JAXA
|
| gptkbp:controls |
Digital control system
|
| gptkbp:diameter |
4 meters
|
| gptkbp:engine_type |
Liquid-fueled
|
| gptkbp:events |
Successful
|
| gptkbp:first_flight |
2001-08-29
2019-01-18 |
| gptkbp:guidance_system |
Inertial navigation system
|
| gptkbp:height |
53 meters
|
| https://www.w3.org/2000/01/rdf-schema#label |
H-IIA 283
|
| gptkbp:launch_date |
2019-01-18
|
| gptkbp:launch_site |
gptkb:Tanegashima_Space_Center
gptkb:JAXA |
| gptkbp:launch_vehicle |
gptkb:H-IIA
300,000 kg |
| gptkbp:launched |
283
|
| gptkbp:manufacturer |
gptkb:Mitsubishi_Heavy_Industries
|
| gptkbp:mass |
200,000 kg
|
| gptkbp:mission |
Commercial
Geostationary orbit Communications satellite deployment |
| gptkbp:number_of_stages |
gptkb:LE-5_B_engine
2 LE-7 A engine |
| gptkbp:reliability |
98%
|
| gptkbp:seating_capacity |
gptkb:DSN-1_satellite
4,000 kg to geostationary transfer orbit |
| gptkbp:status |
Retired
|
| gptkbp:succeeded_by |
gptkb:theorem
|