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gptkbp:instance_of
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gptkb:rocket
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gptkbp:bfsLayer
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4
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gptkbp:bfsParent
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gptkb:JAXA
gptkb:Japanese_Aerospace_Exploration_Agency
gptkb:Japanese_Aerospace_Exploration_Agency_(JAXA)
gptkb:Japan_Aerospace_Exploration_Agency_(JAXA)
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|
gptkbp:collaborations
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Various international payloads
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|
gptkbp:debut_year
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Multiple launches since 2004
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|
gptkbp:design
|
To launch satellites into orbit
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|
gptkbp:developer
|
gptkb:1994
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gptkbp:diameter
|
4 meters
|
|
gptkbp:elevation
|
53 meters
220,000 kg
|
|
gptkbp:engine
|
Staged combustion cycle
|
|
gptkbp:engine_type
|
gptkb:LE-7_A
|
|
gptkbp:events
|
Few failures recorded
Over 30 successful launches
|
|
gptkbp:first_flight
|
gptkb:2004
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gptkbp:fuel_type
|
Liquid hydrogen and liquid oxygen
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|
gptkbp:height
|
53 meters
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
H-IIA 239
|
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gptkbp:launch_date
|
Regular launches
|
|
gptkbp:launch_site
|
gptkb:Tanegashima_Space_Center
JAXA control center
Japan Aerospace Exploration Agency (JAXA
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|
gptkbp:launch_vehicle
|
4 meters
Expendable launch vehicle
White and orange
H-II family
Two-stage design
High performance for various missions
Part of Japan's space program history.
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gptkbp:launched
|
Various configurations available
|
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gptkbp:manufacturer
|
gptkb:Mitsubishi_Heavy_Industries
|
|
gptkbp:market
|
Approximately $90 million
|
|
gptkbp:mission
|
Satellite launches, interplanetary missions
|
|
gptkbp:notable_album
|
gptkb:Hayabusa_mission
|
|
gptkbp:number_of_stages
|
gptkb:LE-5_B
2
2 LE-7 A engines
|
|
gptkbp:operational_area
|
2004 to present
|
|
gptkbp:operational_status
|
Active
|
|
gptkbp:propulsion
|
1,000 k N
|
|
gptkbp:reliability
|
Proven track record
|
|
gptkbp:seating_capacity
|
gptkb:Akasaki_satellite
10,000 kg
4,000 kg
Composite material
Integrated at Tanegashima
Multiple payload configurations available
|
|
gptkbp:succeeded_by
|
gptkb:High
|
|
gptkbp:successor
|
gptkb:H-IIB
|
|
gptkbp:supports
|
Specialized ground support systems
|