Statements (28)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:satellite
|
| gptkbp:countryOfOrigin |
gptkb:Japan
|
| gptkbp:developedBy |
gptkb:NASDA
|
| gptkbp:engine |
gptkb:LE-7
|
| gptkbp:failedLaunches |
2
|
| gptkbp:familyMember |
gptkb:H-IIA
gptkb:H-IIB gptkb:H-II |
| gptkbp:firstFlight |
1994-02-03
|
| gptkbp:launched |
7
|
| gptkbp:launchSite |
gptkb:Tanegashima_Space_Center
|
| gptkbp:manufacturer |
gptkb:Mitsubishi_Heavy_Industries
|
| gptkbp:numberOfLaunches |
5
|
| gptkbp:numberOfStages |
gptkb:LE-5A
2 |
| gptkbp:operator |
gptkb:NASDA
|
| gptkbp:pages |
https://en.wikipedia.org/wiki/H-II
|
| gptkbp:payloadToGTO |
4,000 kg
|
| gptkbp:payloadToLEO |
10,000 kg
|
| gptkbp:propulsion |
gptkb:water
|
| gptkbp:retired |
1999
|
| gptkbp:status |
retired
|
| gptkbp:successor |
gptkb:H-IIA_rocket
|
| gptkbp:usedFor |
launching satellites
launching spacecraft |
| gptkbp:bfsParent |
gptkb:H-IIA_rocket
|
| gptkbp:bfsLayer |
6
|
| https://www.w3.org/2000/01/rdf-schema#label |
H-II rocket family
|