|
gptkbp:instance_of
|
gptkb:Space_Launch_System
gptkb:Team_Rocket
|
|
gptkbp:collaboration
|
NASA, JAXA
|
|
gptkbp:configuration
|
multiple configurations available
|
|
gptkbp:country
|
gptkb:Japan
|
|
gptkbp:current_status
|
in service
|
|
gptkbp:debut
|
gptkb:2001
August 29, 2001
|
|
gptkbp:diameter
|
4 meters
|
|
gptkbp:engine_type
|
gptkb:Team_Rocket
gptkb:LE-7_A
|
|
gptkbp:first_flight
|
gptkb:2001
August 29, 2001
2001-08-29
|
|
gptkbp:flight_style
|
gptkb:45
|
|
gptkbp:height
|
53 meters
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
H-IIA
|
|
gptkbp:launch_date
|
approximately 2-3 per year
|
|
gptkbp:launch_price
|
approximately $90 million
|
|
gptkbp:launch_site
|
gptkb:Tanegashima_Space_Center
|
|
gptkbp:launch_vehicle
|
2 or 4
|
|
gptkbp:launched
|
over 40
|
|
gptkbp:manufacturer
|
gptkb:Mitsubishi_Heavy_Industries
|
|
gptkbp:notable_launches
|
gptkb:Akasaki
gptkb:Hayabusa
gptkb:GCOM-W1_satellite
gptkb:Hayabusa_mission
gptkb:Akasaki_satellite
gptkb:GOSAT
gptkb:H-IIA_202
gptkb:H-IIA_204
|
|
gptkbp:number_of_stages
|
gptkb:LE-5_B
gptkb:LE-7_A
2
2 stages
|
|
gptkbp:operational_status
|
active
operational
|
|
gptkbp:payload_capacity
|
6 tons
10,000 kg
4,000 kg
15 tons
4 meters in diameter
4,000 kg to geostationary transfer orbit
15 tons to low Earth orbit
|
|
gptkbp:primary_use
|
commercial satellite launches
|
|
gptkbp:production_status
|
mature
|
|
gptkbp:reliability
|
high reliability
|
|
gptkbp:success_rate
|
98%
over 90%
|
|
gptkbp:type
|
gptkb:Space_Launch_System
|
|
gptkbp:used_for
|
satellite launches
|
|
gptkbp:bfsParent
|
gptkb:Tanegashima_Space_Center
gptkb:JAXA
gptkb:Japanese_Aerospace_Exploration_Agency
gptkb:Japan_Aerospace_Exploration_Agency
gptkb:Japanese_Aerospace_Exploration_Agency_(JAXA)
gptkb:Japan_Aerospace_Exploration_Agency_(JAXA)
gptkb:H-IIA_204
gptkb:H-IIA_205
|
|
gptkbp:bfsLayer
|
4
|