|
gptkbp:instance_of
|
gptkb:rocket
|
|
gptkbp:bfsLayer
|
4
|
|
gptkbp:bfsParent
|
gptkb:JAXA
gptkb:Japanese_Aerospace_Exploration_Agency
gptkb:Japanese_Aerospace_Exploration_Agency_(JAXA)
gptkb:Japan_Aerospace_Exploration_Agency_(JAXA)
|
|
gptkbp:controls
|
Digital control system
|
|
gptkbp:debut_year
|
Multiple successful launches
|
|
gptkbp:diameter
|
4 meters
|
|
gptkbp:engine_type
|
gptkb:LE-7_A
|
|
gptkbp:events
|
Over 90%
|
|
gptkbp:first_flight
|
2004-08-29
2001-08-29
2019-01-18
|
|
gptkbp:fuel_type
|
gptkb:RP-1/_LOX
Liquid hydrogen and liquid oxygen
|
|
gptkbp:guidance_system
|
Inertial navigation system
|
|
gptkbp:height
|
53 meters
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
H-IIA 238
|
|
gptkbp:launch_date
|
gptkb:television_series
2014-02-24
|
|
gptkbp:launch_site
|
gptkb:Tanegashima_Space_Center
Japan Aerospace Exploration Agency (JAXA
|
|
gptkbp:launch_vehicle
|
gptkb:H-IIA
Expendable launch vehicle
|
|
gptkbp:launched
|
gptkb:Akasaki_satellite
38
Varies by mission
|
|
gptkbp:manufacturer
|
gptkb:Mitsubishi_Heavy_Industries
|
|
gptkbp:market
|
Approximately $90 million
|
|
gptkbp:mission
|
Satellite deployment
Geostationary transfer orbit
|
|
gptkbp:notable_album
|
H-IIA 238 launched Akasaki satellite.
|
|
gptkbp:number_of_stages
|
gptkb:LE-5_B
gptkb:LE-5_B_engine
2
LE-7 A engine
|
|
gptkbp:operational_status
|
Retired
|
|
gptkbp:produced_by
|
Operational
|
|
gptkbp:propulsion
|
1,000 k N
|
|
gptkbp:release_region
|
gptkb:battle
|
|
gptkbp:reliability
|
98%
Proven
|
|
gptkbp:seating_capacity
|
15 meters
4 meters
10,000 kg
4,000 kg
4 meters in diameter
4,000 kg to geostationary transfer orbit
|
|
gptkbp:setting
|
gptkb:H-IIA_202
|
|
gptkbp:social_structure
|
Liquid Oxygen
|
|
gptkbp:succeeded_by
|
gptkb:High
38
|