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gptkbp:instance_of
|
gptkb:Team_Rocket
|
|
gptkbp:collaboration
|
Various international satellite operators
|
|
gptkbp:configuration
|
gptkb:H-IIA_202
|
|
gptkbp:debut
|
Successful launches since 2004
|
|
gptkbp:diameter
|
4 meters
|
|
gptkbp:engine_configuration
|
Two main engines
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|
gptkbp:engine_type
|
gptkb:Rocketdyne_RS-37
|
|
gptkbp:first_flight
|
gptkb:2004
|
|
gptkbp:guidance_system
|
Inertial navigation system
|
|
gptkbp:has_programs
|
H-IIA development program
|
|
gptkbp:height
|
53 meters
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
H-IIA 246 rocket
|
|
gptkbp:launch_date
|
gptkb:Regular
2021-03-01
2004-08-29
|
|
gptkbp:launch_platform
|
gptkb:Mitsubishi_Heavy_Industries
|
|
gptkbp:launch_price
|
Approximately $90 million
|
|
gptkbp:launch_site
|
gptkb:Tanegashima_Space_Center
|
|
gptkbp:launch_vehicle
|
gptkb:H-IIA
Expendable launch system
Two-stage design
|
|
gptkbp:launched
|
gptkb:Multiple
Over 30
|
|
gptkbp:manufacturer
|
gptkb:Mitsubishi_Heavy_Industries
|
|
gptkbp:mission
|
Satellite deployment
|
|
gptkbp:notable_achievements
|
Successful deployment of multiple satellites.
|
|
gptkbp:notable_mission
|
Communications satellites
|
|
gptkbp:number_of_stages
|
2
|
|
gptkbp:operational_status
|
Active
|
|
gptkbp:operational_use
|
Satellite launches for various purposes
|
|
gptkbp:payload_capacity
|
4 meters in diameter
Commercial satellites
4,000 kg to geostationary transfer orbit
|
|
gptkbp:primary_user
|
Japan Aerospace Exploration Agency (JAXA
|
|
gptkbp:propulsion
|
Liquid hydrogen and liquid oxygen
1,000 k N
|
|
gptkbp:reliability
|
Very reliable
|
|
gptkbp:success_rate
|
gptkb:High
|
|
gptkbp:bfsParent
|
gptkb:Tanegashima_Space_Center
|
|
gptkbp:bfsLayer
|
4
|