Statements (25)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:configuration |
solid-fueled
|
| gptkbp:countryOfOrigin |
gptkb:Japan
|
| gptkbp:derivedFrom |
gptkb:M-V_rocket
|
| gptkbp:diameter |
2.6 m
|
| gptkbp:firstFlight |
2013-09-14
|
| https://www.w3.org/2000/01/rdf-schema#label |
Epsilon rocket family
|
| gptkbp:launchSite |
gptkb:Uchinoura_Space_Center
|
| gptkbp:length |
24.4 m
|
| gptkbp:manufacturer |
gptkb:JAXA
gptkb:IHI_Aerospace |
| gptkbp:mass |
91,000 kg
|
| gptkbp:notableMission |
gptkb:Innovative_Satellite_Technology_Demonstration-1
ASNARO-2 Hisaki (SPRINT-A) |
| gptkbp:numberOfStages |
3
4 |
| gptkbp:payloadToLEO |
1200 kg
|
| gptkbp:payloadToSSO |
590 kg
|
| gptkbp:predecessor |
gptkb:Mu_rocket_family
|
| gptkbp:purpose |
launch small satellites
|
| gptkbp:status |
active
|
| gptkbp:website |
https://www.jaxa.jp/projects/rockets/epsilon/index_e.html
|
| gptkbp:bfsParent |
gptkb:Epsilon_S_rocket
|
| gptkbp:bfsLayer |
7
|