|
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_type
|
gptkb:LE-7_A
|
|
gptkbp:first_flight
|
49
2001-08-29
|
|
gptkbp:fuel_type
|
Liquid hydrogen and liquid oxygen
|
|
gptkbp:height
|
53 meters
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
H-IIA 249
|
|
gptkbp:launch_date
|
2022-03-30
2019-01-18
|
|
gptkbp:launch_site
|
gptkb:Tanegashima_Space_Center
|
|
gptkbp:launch_vehicle
|
gptkb:H-IIA
|
|
gptkbp:manufacturer
|
gptkb:Mitsubishi_Heavy_Industries
|
|
gptkbp:mission
|
commercial
Communications satellite deployment
geostationary transfer orbit
|
|
gptkbp:mission_duration
|
gptkb:unknown
|
|
gptkbp:number_of_stages
|
2
|
|
gptkbp:operator
|
gptkb:Mitsubishi_Heavy_Industries
|
|
gptkbp:propulsion
|
1,000 k N
|
|
gptkbp:reliability
|
98%
|
|
gptkbp:seating_capacity
|
gptkb:Akasaki
4,000 kg to geostationary transfer orbit
|
|
gptkbp:succeeded_by
|
gptkb:theorem
|