gptkbp:instance_of
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gptkb:Space_Launch_System
gptkb:Team_Rocket
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gptkbp:control_system
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Inertial navigation system
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gptkbp:engine_type
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gptkb:LE-7_A
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gptkbp:first_flight
|
gptkb:2001
gptkb:2004
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gptkbp:flight_style
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multiple
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gptkbp:fuel_type
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Liquid hydrogen and liquid oxygen
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gptkbp:has_programs
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H-IIA program
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gptkbp:height
|
53 meters
|
https://www.w3.org/2000/01/rdf-schema#label
|
H-IIA 265
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gptkbp:launch_date
|
2014-02-24
Approximately 2-3 per year
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gptkbp:launch_site
|
gptkb:Tanegashima_Space_Center
|
gptkbp:launch_vehicle
|
gptkb:H-IIA
|
gptkbp:launched
|
gptkb:Hayabusa_spacecraft
gptkb:Akasaki_satellite
Over 40
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gptkbp:manufacturer
|
gptkb:Mitsubishi_Heavy_Industries
|
gptkbp:notable_mission
|
gptkb:Akasaki
gptkb:Hayabusa
gptkb:GCOM-W1
gptkb:H-II_Transfer_Vehicle
|
gptkbp:number_of_stages
|
2
|
gptkbp:operational_status
|
Active
active
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gptkbp:payload_capacity
|
4 meters
1,500 kg
4,000 kg
10,000 kg to low Earth orbit
|
gptkbp:propulsion
|
1,000 k N
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gptkbp:reliability
|
gptkb:High
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gptkbp:success_rate
|
gptkb:High
over 90%
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gptkbp:bfsParent
|
gptkb:JAXA
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gptkbp:bfsLayer
|
4
|