Statements (30)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:satellite
|
| gptkbp:boosters |
solid rocket boosters
|
| gptkbp:configurationVariants |
gptkb:H-IIA_2022
gptkb:H-IIA_2024 gptkb:H-IIA_204 gptkb:H-IIA_202 |
| gptkbp:countryOfOrigin |
gptkb:Japan
|
| gptkbp:diameter |
4 m
|
| gptkbp:family |
gptkb:H-II_family
|
| gptkbp:firstFlight |
2001-08-29
|
| gptkbp:height |
53 m
|
| https://www.w3.org/2000/01/rdf-schema#label |
Japanese H-IIA rocket
|
| gptkbp:launchSite |
gptkb:Tanegashima_Space_Center
|
| gptkbp:manufacturer |
gptkb:Mitsubishi_Heavy_Industries
|
| gptkbp:mass |
285,000 kg
|
| gptkbp:notableMission |
gptkb:Kaguya_(SELENE)_lunar_orbiter
gptkb:Akatsuki_Venus_probe gptkb:Hayabusa2_asteroid_mission |
| gptkbp:numberOfStages |
2
|
| gptkbp:operator |
gptkb:JAXA
|
| gptkbp:payloadToGTO |
4,100 kg
|
| gptkbp:payloadToLEO |
10,000 kg
|
| gptkbp:propulsion |
liquid oxygen
liquid hydrogen |
| gptkbp:status |
active
|
| gptkbp:usedFor |
interplanetary missions
satellite launches |
| gptkbp:website |
https://www.mhi.com/products/space/h2a.html
|
| gptkbp:bfsParent |
gptkb:J1_platform
|
| gptkbp:bfsLayer |
7
|