|
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:height
|
53 meters
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
H-IIA 206
|
|
gptkbp:launch_date
|
2006-02-24
2001-08-29
|
|
gptkbp:launch_site
|
gptkb:Tanegashima_Space_Center
|
|
gptkbp:launch_vehicle
|
gptkb:H-IIA
2
|
|
gptkbp:launched
|
over 40
|
|
gptkbp:manufacturer
|
gptkb:Mitsubishi_Heavy_Industries
|
|
gptkbp:market
|
approximately $90 million
|
|
gptkbp:mission
|
commercial
geostationary transfer orbit
|
|
gptkbp:mission_duration
|
gptkb:unknown
|
|
gptkbp:notable_album
|
gptkb:H-II_Transfer_Vehicle_(HTV)
gptkb:GCOM-W1_satellite
gptkb:Akasaki_satellite
gptkb:H-IIA_202
gptkb:H-IIA_204
|
|
gptkbp:number_of_stages
|
2
1,000 k N
150 k N
|
|
gptkbp:operator
|
gptkb:Mitsubishi_Heavy_Industries
|
|
gptkbp:primary_user
|
gptkb:Japan_Aerospace_Exploration_Agency_(JAXA)
|
|
gptkbp:seating_capacity
|
4,000 kg to geostationary transfer orbit
DSN-1
|
|
gptkbp:succeeded_by
|
gptkb:theorem
over 90%
|