Statements (24)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:spacecraft
|
| gptkbp:control_system |
Inertial navigation system
|
| gptkbp:design_purpose |
Small satellite launch
|
| gptkbp:development_cost |
Approximately $100 million
|
| gptkbp:diameter |
2.5 meters
|
| gptkbp:first_flight |
September 14, 2013
|
| gptkbp:guidance_system |
GPS-based guidance
|
| gptkbp:height |
24 meters
|
| https://www.w3.org/2000/01/rdf-schema#label |
Epsilon S
|
| gptkbp:launch_date |
1-2 times per year
|
| gptkbp:launch_mass |
90 tons
|
| gptkbp:launch_site |
gptkb:Uchinoura_Space_Center
|
| gptkbp:launch_vehicle |
gptkb:Epsilon_rocket_family
|
| gptkbp:manufacturer |
gptkb:Mitsubishi_Heavy_Industries
|
| gptkbp:notable_launches |
gptkb:H-IIA_202
|
| gptkbp:number_of_stages |
gptkb:3
|
| gptkbp:operational_status |
Active
|
| gptkbp:payload_capacity |
Composite material
1,200 kg to low Earth orbit |
| gptkbp:propulsion |
Solid rocket fuel
|
| gptkbp:reliability |
98%
|
| gptkbp:success_rate |
gptkb:High
|
| gptkbp:bfsParent |
gptkb:Epsilon_rocket
|
| gptkbp:bfsLayer |
5
|