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gptkbp:instance_of
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gptkb:aircraft
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:collaborations
|
NASA, ESA
|
|
gptkbp:controls
|
inertial guidance system
|
|
gptkbp:debut_year
|
2021-03-30
2001-08-29
operational since 2001
|
|
gptkbp:diameter
|
4 meters
|
|
gptkbp:engine_type
|
gptkb:LE-7_A
|
|
gptkbp:events
|
Successful
|
|
gptkbp:first_flight
|
gptkb:2001
gptkb:2022
over 30
|
|
gptkbp:height
|
53 meters
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
H-IIA 209
|
|
gptkbp:launch_date
|
2004-02-21
2014-02-22
approximately 2-3 launches per year
|
|
gptkbp:launch_site
|
gptkb:Tanegashima_Space_Center
Japan Aerospace Exploration Agency (JAXA
|
|
gptkbp:launch_vehicle
|
gptkb:H-IIA
gptkb:H-IIA_202
|
|
gptkbp:launched
|
gptkb:musical
gptkb:Akasaki_satellite
29
available for commercial payloads
|
|
gptkbp:manufacturer
|
gptkb:Mitsubishi_Heavy_Industries
|
|
gptkbp:mission
|
Successful
Satellite launch
Geostationary transfer orbit
Geostationary satellite deployment
|
|
gptkbp:notable_album
|
H-IIA 209 launched Akasaki satellite
|
|
gptkbp:number_of_stages
|
2
LE-7 A engine
H M7 A engine
|
|
gptkbp:operator
|
gptkb:Mitsubishi_Heavy_Industries
|
|
gptkbp:orbital_inclination
|
Geostationary orbit
|
|
gptkbp:propulsion
|
liquid hydrogen and liquid oxygen
|
|
gptkbp:reliability
|
98%
highly reliable
|
|
gptkbp:seating_capacity
|
gptkb:DSN-1_satellite
10,000 kg to geostationary transfer orbit
4,000 kg to geostationary transfer orbit
DSN-1
4,000 kg to GTO
|
|
gptkbp:succeeded_by
|
gptkb:musical
gptkb:theorem
over 90%
|