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gptkbp:instance_of
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gptkb:aircraft
gptkb:rocket
|
|
gptkbp:bfsLayer
|
4
|
|
gptkbp:bfsParent
|
gptkb:JAXA
gptkb:Japanese_Aerospace_Exploration_Agency
gptkb:Japanese_Aerospace_Exploration_Agency_(JAXA)
gptkb:Japan_Aerospace_Exploration_Agency_(JAXA)
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|
gptkbp:debut_year
|
multiple launches since introduction
|
|
gptkbp:developer
|
developed from H-II rocket
|
|
gptkbp:diameter
|
4 meters
|
|
gptkbp:engine_type
|
gptkb:rocket
|
|
gptkbp:first_flight
|
gptkb:2001
gptkb:2004
|
|
gptkbp:fuel_type
|
kerosene and liquid oxygen
|
|
gptkbp:guidance_system
|
inertial guidance system
|
|
gptkbp:height
|
53 meters
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
H-IIA 231
|
|
gptkbp:launch_date
|
several launches per year
|
|
gptkbp:launch_site
|
gptkb:Tanegashima_Space_Center
gptkb:JAXA
|
|
gptkbp:launch_vehicle
|
gptkb:H-IIA
|
|
gptkbp:launched
|
gptkb:Akasaki_satellite
|
|
gptkbp:manufacturer
|
gptkb:Mitsubishi_Heavy_Industries
|
|
gptkbp:market
|
approximately $90 million
|
|
gptkbp:notable_album
|
H-IIA 231 launched Akasaki satellite
|
|
gptkbp:number_of_stages
|
2
|
|
gptkbp:operational_status
|
active
|
|
gptkbp:propulsion
|
1,000 k N
|
|
gptkbp:purpose
|
gptkb:spacecraft
|
|
gptkbp:reliability
|
high
|
|
gptkbp:seating_capacity
|
4 meters in diameter
10,000 kg to geostationary transfer orbit
4,000 kg to geostationary transfer orbit
|
|
gptkbp:setting
|
standard configuration
|
|
gptkbp:succeeded_by
|
multiple
over 90%
|