Statements (28)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:satellite
|
| gptkbp:book |
gptkb:LE-5
|
| gptkbp:countryOfOrigin |
gptkb:Japan
|
| gptkbp:derivedFrom |
gptkb:N-II_rocket
|
| gptkbp:diameter |
2.44 m
|
| gptkbp:failedLaunches |
1
|
| gptkbp:firstFlight |
1986-08-13
|
| gptkbp:height |
43.9 m
|
| gptkbp:lastFlight |
1992-02-18
|
| gptkbp:launchSite |
gptkb:Tanegashima_Space_Center
|
| gptkbp:manufacturer |
gptkb:Mitsubishi_Heavy_Industries
|
| gptkbp:mass |
260,000 kg
|
| gptkbp:numberOfLaunches |
8
9 |
| gptkbp:numberOfStages |
gptkb:LE-7
2 |
| gptkbp:pages |
https://en.wikipedia.org/wiki/H-I
|
| gptkbp:payloadToGTO |
770 kg
|
| gptkbp:payloadToLEO |
2,000 kg
|
| gptkbp:propulsion |
liquid oxygen
liquid hydrogen solid fuel (first stage boosters) |
| gptkbp:status |
retired
|
| gptkbp:successor |
gptkb:H-II_rocket
|
| gptkbp:usedBy |
gptkb:NASDA
|
| gptkbp:bfsParent |
gptkb:National_Space_Development_Agency_of_Japan
|
| gptkbp:bfsLayer |
6
|
| https://www.w3.org/2000/01/rdf-schema#label |
H-I rocket
|