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gptkbp:instance_of
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gptkb:Team_Rocket
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|
gptkbp:collaboration
|
with various space agencies
|
|
gptkbp:collaborative_projects
|
with international partners
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|
gptkbp:configuration
|
gptkb:H-IIA_202
|
|
gptkbp:control_system
|
advanced guidance system
|
|
gptkbp:debut
|
part of the H-IIA program
|
|
gptkbp:design
|
based on earlier H-II designs
|
|
gptkbp:development
|
ongoing improvements
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|
gptkbp:diameter
|
4 meters
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gptkbp:engine_type
|
gptkb:Team_Rocket
|
|
gptkbp:first_flight
|
2004-09-29
|
|
gptkbp:fuel_type
|
kerosene and liquid oxygen
|
|
gptkbp:ground_support_equipment
|
specialized launch pads
|
|
gptkbp:height
|
53 meters
|
|
gptkbp:historical_significance
|
important for Japan's space exploration
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
H-IIA 292 rocket
|
|
gptkbp:launch_count
|
multiple successful launches
|
|
gptkbp:launch_date
|
2004-09-29
regular launches
|
|
gptkbp:launch_platform
|
gptkb:JAXA
|
|
gptkbp:launch_price
|
competitive pricing
|
|
gptkbp:launch_site
|
gptkb:Tanegashima_Space_Center
|
|
gptkbp:launch_vehicle
|
gptkb:H-IIA_series
state-of-the-art technology
part of the H-II family
|
|
gptkbp:launch_vehicles_used
|
for various missions
|
|
gptkbp:legacy
|
contributed to Japan's space capabilities
|
|
gptkbp:manufacturer
|
gptkb:Mitsubishi_Heavy_Industries
|
|
gptkbp:mission
|
high success rate
|
|
gptkbp:notable_launches
|
H-IIA 292 launch of the Akasaki satellite
|
|
gptkbp:notable_mission
|
various scientific missions
|
|
gptkbp:number_of_flights
|
multiple
|
|
gptkbp:number_of_stages
|
2
|
|
gptkbp:operational_period
|
2004 to 2020
|
|
gptkbp:operational_status
|
retired
|
|
gptkbp:part_of
|
Japan's national space program
|
|
gptkbp:payload_capacity
|
commercial satellites
4,000 kg to geostationary transfer orbit
|
|
gptkbp:payload_deployment
|
in geostationary orbit
|
|
gptkbp:payload_types
|
commercial and scientific payloads
|
|
gptkbp:primary_use
|
gptkb:Space_Launch_System
|
|
gptkbp:propulsion
|
1,000 k N
|
|
gptkbp:reliability
|
high
|
|
gptkbp:safety_record
|
excellent
|
|
gptkbp:spacecraft_integration
|
integrated at Tanegashima
|
|
gptkbp:success_rate
|
over 90%
|
|
gptkbp:successor
|
gptkb:H-IIA_202_series
|
|
gptkbp:technical_innovation
|
improved reliability features
|
|
gptkbp:technical_specifications
|
detailed engineering data available.
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gptkbp:bfsParent
|
gptkb:Tanegashima_Space_Center
|
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gptkbp:bfsLayer
|
4
|