Statements (29)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
rocket variant
|
| gptkbp:boosters |
solid rocket boosters (SRB-A)
|
| gptkbp:configuration |
various (e.g., 202, 204, 2022, 2024, 202F, etc.)
|
| gptkbp:countryOfOrigin |
gptkb:Japan
|
| gptkbp:diameter |
4 m
|
| gptkbp:firstFlight |
2001
|
| https://www.w3.org/2000/01/rdf-schema#label |
H-IIA rocket variant
|
| gptkbp:launchSite |
gptkb:Tanegashima_Space_Center
|
| gptkbp:length |
53 m (varies by variant)
|
| gptkbp:manufacturer |
gptkb:Mitsubishi_Heavy_Industries
|
| gptkbp:notableMission |
gptkb:Hayabusa2
gptkb:Kaguya_(SELENE) gptkb:GOSAT gptkb:Himawari-8 gptkb:Akatsuki |
| gptkbp:numberOfStages |
2
|
| gptkbp:operator |
gptkb:JAXA
|
| gptkbp:partOf |
H-IIA rocket family
|
| gptkbp:payloadToGTO |
up to 6,000 kg
|
| gptkbp:payloadToLEO |
up to 15,000 kg
|
| gptkbp:propulsion |
liquid oxygen
liquid hydrogen |
| gptkbp:status |
active
|
| gptkbp:successRate |
over 97%
|
| gptkbp:usedFor |
satellite launches
space probe launches |
| gptkbp:website |
https://www.mhi.com/products/space/h2a.html
|
| gptkbp:bfsParent |
gptkb:H-IIA_202
|
| gptkbp:bfsLayer |
6
|