Statements (22)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:countryOfOrigin |
gptkb:Japan
|
| gptkbp:diameter |
2.5 m
|
| gptkbp:firstFlight |
2001-09-10
|
| gptkbp:height |
30.7 m
|
| https://www.w3.org/2000/01/rdf-schema#label |
Mu-V
|
| gptkbp:lastFlight |
2006-09-23
|
| gptkbp:launchSite |
gptkb:Uchinoura_Space_Center
|
| gptkbp:manufacturer |
Mu Rocket Development Group
|
| gptkbp:mass |
137,500 kg
|
| gptkbp:numberOfLaunches |
7
|
| gptkbp:numberOfStages |
3
|
| gptkbp:payload |
gptkb:Hayabusa
gptkb:ASTRO-E |
| gptkbp:payloadToLEO |
1,800 kg
|
| gptkbp:payloadToSSO |
1,300 kg
|
| gptkbp:predecessor |
gptkb:Mu-3S-II
|
| gptkbp:status |
retired
|
| gptkbp:successor |
Epsilon (rocket)
|
| gptkbp:usedFor |
launching scientific satellites
|
| gptkbp:bfsParent |
gptkb:M-V_rocket_family
|
| gptkbp:bfsLayer |
7
|