Statements (28)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
Japanese launch vehicle
|
| gptkbp:book |
gptkb:LE-5A
|
| gptkbp:countryOfOrigin |
gptkb:Japan
|
| gptkbp:diameter |
4.0 m
|
| gptkbp:failedLaunches |
2
|
| gptkbp:firstFlight |
1994-02-03
|
| gptkbp:height |
49.0 m
|
| https://www.w3.org/2000/01/rdf-schema#label |
H-II
|
| gptkbp:lastFlight |
1999-11-15
|
| gptkbp:launchSite |
gptkb:Tanegashima_Space_Center
|
| gptkbp:manufacturer |
gptkb:NASDA
|
| gptkbp:mass |
260,000 kg
|
| gptkbp:notableMission |
gptkb:ADEOS_I
gptkb:ETS-VI gptkb:Kakehashi |
| gptkbp:numberOfLaunches |
5
7 |
| gptkbp:numberOfStages |
gptkb:LE-7
2 |
| gptkbp:payloadToGTO |
4,000 kg
|
| gptkbp:payloadToLEO |
10,000 kg
|
| gptkbp:predecessor |
gptkb:H-I
|
| gptkbp:propulsion |
gptkb:water
|
| gptkbp:status |
retired
|
| gptkbp:successor |
gptkb:H-IIA
|
| gptkbp:usedFor |
satellite launches
|
| gptkbp:bfsParent |
gptkb:H-IIA
|
| gptkbp:bfsLayer |
6
|