|
gptkbp:instance_of
|
gptkb:aircraft
gptkb:rocket
|
|
gptkbp:collaborations
|
NASA, ESA
|
|
gptkbp:controls
|
digital
|
|
gptkbp:debut_year
|
gptkb:2001
gptkb:2023
multiple successful launches
|
|
gptkbp:developer
|
gptkb:H-IIA_series
|
|
gptkbp:diameter
|
4 meters
|
|
gptkbp:elevation
|
4 meters
53 meters
|
|
gptkbp:engine
|
gptkb:musical
gptkb:LE-7_A
staged combustion cycle
|
|
gptkbp:engine_type
|
gptkb:rocket
gptkb:LE-7_A
gptkb:item
|
|
gptkbp:equipment
|
gptkb:battle
|
|
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:hospital
|
|
gptkbp:height
|
53 meters
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
H-IIA 202
|
|
gptkbp:is_used_for
|
gptkb:spacecraft
gptkb:GCOM-C1
gptkb:GCOM-W1
gptkb:Bepi_Colombo
Launching satellites
|
|
gptkbp:launch_date
|
several per year
|
|
gptkbp:launch_site
|
gptkb:Tanegashima_Space_Center
gptkb:JAXA
|
|
gptkbp:launch_vehicle
|
high reliability
medium-lift
two-stage rocket
220,000 kg
H-II series
288,000 kg
|
|
gptkbp:launched
|
gptkb:30
gptkb:Akasaki_satellite
|
|
gptkbp:manufacturer
|
gptkb:Mitsubishi_Heavy_Industries
|
|
gptkbp:market
|
approximately $90 million
|
|
gptkbp:mass
|
220,000 kg
|
|
gptkbp:mission
|
over 90%
planned
communications satellites
commercial, governmental
|
|
gptkbp:notable_album
|
gptkb:Himawari-9
gptkb:Hayabusa2
|
|
gptkbp:number_of_stages
|
2
H M7 B
|
|
gptkbp:operational_status
|
gptkb:2004
active
|
|
gptkbp:origin
|
gptkb:Japan
|
|
gptkbp:part_of
|
gptkb:H-IIA_family
|
|
gptkbp:propulsion
|
1,000 k N
|
|
gptkbp:reliability
|
high
|
|
gptkbp:seating_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:setting
|
two-stage
|
|
gptkbp:succeeded_by
|
over 90%
Approximately 98%
96.7%
|
|
gptkbp:bfsParent
|
gptkb:rocket
|
|
gptkbp:bfsLayer
|
3
|