|
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:diameter
|
4 meters
|
|
gptkbp:engine
|
gptkb:musical
|
|
gptkbp:engine_type
|
gptkb:LE-7_A
|
|
gptkbp:first_flight
|
2021-03-01
2004-08-29
|
|
gptkbp:height
|
53 meters
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
H-IIA 213
|
|
gptkbp:launch_date
|
2019-01-18
|
|
gptkbp:launch_site
|
gptkb:Tanegashima_Space_Center
|
|
gptkbp:launch_vehicle
|
gptkb:H-IIA
gptkb:H-IIA_202
2
|
|
gptkbp:launched
|
gptkb:musical
gptkb:Japan_Aerospace_Exploration_Agency_(JAXA)
|
|
gptkbp:manufacturer
|
gptkb:Mitsubishi_Heavy_Industries
|
|
gptkbp:mission
|
Satellite launch
Geostationary transfer orbit
Earth observation satellite deployment
|
|
gptkbp:mission_duration
|
Not specified
|
|
gptkbp:number_of_stages
|
2
|
|
gptkbp:operator
|
gptkb:Mitsubishi_Heavy_Industries
|
|
gptkbp:seating_capacity
|
gptkb:Akasaki
gptkb:DAICHI-2
10,000 kg
4,000 kg
|
|
gptkbp:setting
|
gptkb:H-IIA_202
|
|
gptkbp:succeeded_by
|
gptkb:theorem
95%
|