|
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:collaborations
|
NASA, ESA
|
|
gptkbp:controls
|
digital control system
|
|
gptkbp:debut_year
|
operational since 2001
|
|
gptkbp:design
|
15 years
|
|
gptkbp:diameter
|
4 meters
|
|
gptkbp:engine_type
|
gptkb:LE-7_A
|
|
gptkbp:first_flight
|
gptkb:2001
2004-08-29
|
|
gptkbp:fuel_type
|
cryogenic
|
|
gptkbp:guidance_system
|
inertial guidance system
|
|
gptkbp:has_programs
|
H-II program
|
|
gptkbp:height
|
53 meters
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
H-IIA 211
|
|
gptkbp:launch_date
|
gptkb:2021
February 2001
2006-02-18
approximately 2-3 per year
|
|
gptkbp:launch_site
|
gptkb:Tanegashima_Space_Center
gptkb:JAXA
|
|
gptkbp:launch_vehicle
|
gptkb:H-IIA
gptkb:H-IIA_211
expendable launch vehicle
medium-lift
two solid rocket boosters
H-II family
|
|
gptkbp:launched
|
over 40
varies by mission
211 configuration
|
|
gptkbp:manufacturer
|
gptkb:Mitsubishi_Heavy_Industries
|
|
gptkbp:mission
|
gptkb:Akasaki_satellite
over 90%
successful
satellite deployment
direct injection to orbit
|
|
gptkbp:mission_duration
|
gptkb:unknown
|
|
gptkbp:number_of_stages
|
2
|
|
gptkbp:operational_status
|
active
|
|
gptkbp:operator
|
gptkb:Mitsubishi_Heavy_Industries
|
|
gptkbp:primary_source
|
satellite deployment
|
|
gptkbp:propulsion
|
liquid hydrogen and liquid oxygen
1,000 k N
|
|
gptkbp:reliability
|
high
|
|
gptkbp:restoration
|
gptkb:none
|
|
gptkbp:seating_capacity
|
gptkb:H-II_Transfer_Vehicle
4 meters in diameter
4,000 kg to geostationary transfer orbit
DSN-1
commercial, scientific, governmental
done at Tanegashima
|
|
gptkbp:strategic_importance
|
gptkb:0
|
|
gptkbp:succeeded_by
|
gptkb:15
gptkb:theorem
over 90%
|