Statements (28)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
solid-fuel launch vehicle
|
| gptkbp:countryOfOrigin |
gptkb:Japan
|
| gptkbp:derivedFrom |
gptkb:M-V_rocket
|
| gptkbp:diameter |
2.6 m
|
| gptkbp:firstFlight |
2013-09-14
|
| gptkbp:height |
24.4 m
|
| https://www.w3.org/2000/01/rdf-schema#label |
Epsilon rocket
|
| gptkbp:lastFlight |
2023-09-07
|
| gptkbp:launchSite |
gptkb:Uchinoura_Space_Center
|
| gptkbp:manufacturer |
gptkb:JAXA
|
| gptkbp:mass |
91,000 kg
|
| gptkbp:notableMission |
gptkb:ASNARO-2_satellite
gptkb:Hisaki_satellite gptkb:Innovative_Satellite_Technology_Demonstration-1 |
| gptkbp:numberOfLaunches |
5
6 |
| gptkbp:numberOfStages |
3
4 |
| gptkbp:payloadToLEO |
1200 kg
|
| gptkbp:payloadToSSO |
590 kg
|
| gptkbp:propulsion |
gptkb:stone
|
| gptkbp:status |
retired
|
| gptkbp:successor |
gptkb:Epsilon_S_rocket
|
| gptkbp:successRate |
80%
|
| gptkbp:usedFor |
launching scientific satellites
|
| gptkbp:bfsParent |
gptkb:JAXA
gptkb:RP-1 |
| gptkbp:bfsLayer |
5
|