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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:derivedFrom
|
gptkb:H-II_launch_vehicle
|
|
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
|
H-IIA launch vehicle
|
|
gptkbp:launchSite
|
gptkb:Tanegashima_Space_Center
|
|
gptkbp:manufacturer
|
gptkb:Mitsubishi_Heavy_Industries
|
|
gptkbp:mass
|
285,000 kg
|
|
gptkbp:notableMission
|
gptkb:Hayabusa2
gptkb:Kaguya_(SELENE)
gptkb:Himawari-8
gptkb:Akatsuki
|
|
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:successRate
|
over 97%
|
|
gptkbp:usedFor
|
interplanetary missions
satellite launches
|
|
gptkbp:website
|
https://www.mhi.com/products/space/h2a.html
|
|
gptkbp:bfsParent
|
gptkb:IHI_Aerospace
|
|
gptkbp:bfsLayer
|
6
|