|
gptkbp:instance_of
|
gptkb:Space_Launch_System
gptkb:Team_Rocket
|
|
gptkbp:collaboration
|
NASA, ESA
|
|
gptkbp:configuration
|
two-stage
|
|
gptkbp:control_system
|
digital
|
|
gptkbp:country_of_origin
|
gptkb:Japan
|
|
gptkbp:debut
|
gptkb:2001
gptkb:2023
multiple successful launches
|
|
gptkbp:development
|
gptkb:H-IIA_series
|
|
gptkbp:diameter
|
4 meters
|
|
gptkbp:elevation
|
4 meters
53 meters
|
|
gptkbp:engine
|
gptkb:LE-7_A
|
|
gptkbp:engine_configuration
|
staged combustion cycle
|
|
gptkbp:engine_type
|
gptkb:Team_Rocket
gptkb:LE-7_A
gptkb:liquid
|
|
gptkbp:first_flight
|
gptkb:2001
gptkb:2004
2004-08-29
2001-08-29
|
|
gptkbp:fuel_type
|
liquid hydrogen and liquid oxygen
|
|
gptkbp:guidance_system
|
gptkb:navigation_system
|
|
gptkbp:height
|
53 meters
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
H-IIA 202
|
|
gptkbp:launch_date
|
several per year
|
|
gptkbp:launch_mass
|
220,000 kg
288,000 kg
|
|
gptkbp:launch_platform
|
gptkb:JAXA
|
|
gptkbp:launch_price
|
approximately $90 million
|
|
gptkbp:launch_site
|
gptkb:Tanegashima_Space_Center
|
|
gptkbp:launch_vehicle
|
high reliability
medium-lift
two-stage rocket
H-II series
|
|
gptkbp:launched
|
gptkb:30
gptkb:Akasaki_satellite
|
|
gptkbp:manufacturer
|
gptkb:Mitsubishi_Heavy_Industries
|
|
gptkbp:mass
|
220,000 kg
|
|
gptkbp:mission
|
over 90%
planned
|
|
gptkbp:mission_type
|
commercial, governmental
|
|
gptkbp:notable_launches
|
gptkb:Himawari-9
gptkb:Hayabusa2
|
|
gptkbp:notable_mission
|
communications satellites
|
|
gptkbp:number_of_engines
|
gptkb:1
|
|
gptkbp:number_of_stages
|
2
HM7 B
|
|
gptkbp:operational_since
|
gptkb:2004
|
|
gptkbp:operational_status
|
active
|
|
gptkbp:part_of
|
gptkb:H-IIA_family
|
|
gptkbp:payload_capacity
|
gptkb:Himawari_satellites
1,500 kg
6,000 kg
10,000 kg
2,500 kg
4,000 kg
vertical integration
5 meters in diameter
4,000 kg to geostationary transfer orbit
satellites, scientific instruments
4,000 kg to geostationary orbit
|
|
gptkbp:propulsion
|
1,000 k N
|
|
gptkbp:reliability
|
high
|
|
gptkbp:reusable_components
|
no
|
|
gptkbp:success_rate
|
over 90%
Approximately 98%
96.7%
|
|
gptkbp:used_for
|
gptkb:GCOM-C1
gptkb:Space_Launch_System
gptkb:GCOM-W1
gptkb:Bepi_Colombo
Launching satellites
|
|
gptkbp:bfsParent
|
gptkb:Team_Rocket
|
|
gptkbp:bfsLayer
|
3
|