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gptkbp:instance_of
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gptkb:Space_Launch_System
gptkb:Team_Rocket
|
|
gptkbp:collaboration
|
gptkb:Yes
|
|
gptkbp:configuration
|
gptkb:H-IIA_202
|
|
gptkbp:customer_support
|
Comprehensive support offered
|
|
gptkbp:debut
|
gptkb:2021
Multiple successful launches
|
|
gptkbp:diameter
|
4 meters
|
|
gptkbp:engine_type
|
gptkb:LE-7_A
gptkb:liquid
|
|
gptkbp:environmental_impact
|
Minimized emissions
|
|
gptkbp:first_flight
|
gptkb:2001
gptkb:2004
2021-03-30
2004-08-29
|
|
gptkbp:future_plans
|
Continued use for satellite launches
|
|
gptkbp:ground_testing
|
Extensive ground testing conducted
|
|
gptkbp:guidance_system
|
Inertial navigation system
|
|
gptkbp:height
|
53 meters
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
H-IIA 264
|
|
gptkbp:involved_technology
|
Provided to international clients
|
|
gptkbp:launch_date
|
gptkb:Regular
|
|
gptkbp:launch_documentation
|
Detailed documentation provided
|
|
gptkbp:launch_innovation
|
Continuous improvements made
|
|
gptkbp:launch_platform
|
Japan Aerospace Exploration Agency (JAXA
Automated launch control system
Conducted for each mission
|
|
gptkbp:launch_price
|
Approximately $90 million
|
|
gptkbp:launch_record
|
Over 40 launches
|
|
gptkbp:launch_service_provider
|
gptkb:Mitsubishi_Heavy_Industries
|
|
gptkbp:launch_site
|
gptkb:Tanegashima_Space_Center
|
|
gptkbp:launch_vehicle
|
Expendable launch vehicle
H-II family
Two-stage design
|
|
gptkbp:launch_window
|
Varies by mission
|
|
gptkbp:launched
|
gptkb:Akasaki_satellite
Several months
Ground support equipment
|
|
gptkbp:manufacturer
|
gptkb:Mitsubishi_Heavy_Industries
|
|
gptkbp:mission
|
gptkb:JAXA_Mission_Control_Center
High success rate
|
|
gptkbp:mission_duration
|
Varies by mission
|
|
gptkbp:notable_achievements
|
Successful deployment of multiple satellites
|
|
gptkbp:notable_launches
|
H-IIA 264 launched Akasaki satellite
|
|
gptkbp:number_of_engines
|
gptkb:1
|
|
gptkbp:number_of_stages
|
gptkb:Solid_Rocket_Boosters
gptkb:LE-5_A_engine
2
|
|
gptkbp:operational_status
|
Active
|
|
gptkbp:orbital_inclination
|
Geostationary orbit
|
|
gptkbp:partnerships
|
Collaborations with various space agencies
|
|
gptkbp:payload_capacity
|
10,000 kg
4,000 kg
Composite material
10,000 kg to geostationary transfer orbit
Multiple configurations available
4,000 kg to geostationary transfer orbit
Pre-launch integration at Tanegashima
Precise deployment capabilities
|
|
gptkbp:production_status
|
Operational
|
|
gptkbp:propulsion
|
RP-1 and Liquid Oxygen
|
|
gptkbp:purpose
|
Satellite launch
|
|
gptkbp:reliability
|
Proven
|
|
gptkbp:safety_record
|
Good safety record
|
|
gptkbp:specification
|
Detailed specifications available
|
|
gptkbp:success_rate
|
gptkb:High
95%
over 90%
|
|
gptkbp:training_programs
|
Available for clients
|
|
gptkbp:upgrades
|
Planned upgrades for enhanced performance
|
|
gptkbp:user_countries
|
Japan and international clients
|
|
gptkbp:bfsParent
|
gptkb:JAXA
|
|
gptkbp:bfsLayer
|
4
|