|
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:community_involvement
|
JAXA programs
|
|
gptkbp:controls
|
digital control system
|
|
gptkbp:debut_year
|
gptkb:2023
multiple missions
|
|
gptkbp:diameter
|
4 meters
|
|
gptkbp:engine_type
|
gptkb:rocket
gptkb:LE-7_A
|
|
gptkbp:environmental_impact
|
monitored
|
|
gptkbp:events
|
few
high success rate
|
|
gptkbp:first_flight
|
gptkb:2001
|
|
gptkbp:fuel_type
|
liquid hydrogen and liquid oxygen
|
|
gptkbp:guidance_system
|
gptkb:hospital
|
|
gptkbp:healthcare
|
real-time telemetry
|
|
gptkbp:height
|
53 meters
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
H-IIA 250
|
|
gptkbp:launch_date
|
several per year
|
|
gptkbp:launch_site
|
gptkb:Tanegashima_Space_Center
gptkb:JAXA
gptkb:Mitsubishi_Heavy_Industries
mission dependent
|
|
gptkbp:launch_vehicle
|
gptkb:Launch_Complex_1
optional
modular design
expendable launch vehicle
H-II
by specialized vehicle
|
|
gptkbp:launched
|
several months
varies by mission
|
|
gptkbp:manufacturer
|
gptkb:Mitsubishi_Heavy_Industries
|
|
gptkbp:market
|
approximately $90 million
|
|
gptkbp:mass
|
220,000 kg
|
|
gptkbp:mission
|
gptkb:H-II_Transfer_Vehicle_(HTV)
gptkb:Akasaki
gptkb:Hayabusa
gptkb:GCOM-W1
planned
satellite launches
JAXA control center
|
|
gptkbp:mission_duration
|
approximately 30 minutes
|
|
gptkbp:number_of_stages
|
gptkb:LE-5_B_engine
2
LE-7 A engine
|
|
gptkbp:open_to_public
|
limited access to launch sites
|
|
gptkbp:operational_status
|
gptkb:2001
active
|
|
gptkbp:partnerships
|
international collaborations
|
|
gptkbp:primary_user
|
gptkb:Japan_Aerospace_Exploration_Agency_(JAXA)
|
|
gptkbp:produced_by
|
operational
|
|
gptkbp:propulsion
|
4.5
1,000 k N
|
|
gptkbp:recording_location
|
multiple worldwide
|
|
gptkbp:release_region
|
gptkb:battle
|
|
gptkbp:reliability
|
high
|
|
gptkbp:restoration
|
not applicable
|
|
gptkbp:safety_features
|
redundant systems
|
|
gptkbp:seating_capacity
|
10,000 kg
2,500 kg
4,000 kg
4 meters in diameter
done at Tanegashima
|
|
gptkbp:setting
|
two-stage
H-IIA 200, H-IIA 202
|
|
gptkbp:succeeded_by
|
over 90%
|