|
gptkbp:instance_of
|
gptkb:rocket
|
|
gptkbp:bfsLayer
|
4
|
|
gptkbp:bfsParent
|
gptkb:Tanegashima_Space_Center
|
|
gptkbp:challenges
|
overcame significant engineering challenges
|
|
gptkbp:collaborations
|
limited
|
|
gptkbp:community_engagement
|
engaged with the public through events
|
|
gptkbp:debut_year
|
multiple successful launches
|
|
gptkbp:design
|
to launch payloads into space
|
|
gptkbp:developer
|
developed in Japan
|
|
gptkbp:diameter
|
4 meters
|
|
gptkbp:education
|
inspired educational programs in aerospace.
|
|
gptkbp:engine
|
2
|
|
gptkbp:engine_type
|
gptkb:rocket
|
|
gptkbp:environmental_impact
|
low emissions
|
|
gptkbp:events
|
high success rate
|
|
gptkbp:first_flight
|
gptkb:2004
|
|
gptkbp:first_generation
|
gptkb:H-IIB_rocket
|
|
gptkbp:fuel_type
|
liquid hydrogen and liquid oxygen
|
|
gptkbp:guidance_system
|
inertial guidance system
|
|
gptkbp:height
|
53 meters
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
H-IIA 254 rocket
|
|
gptkbp:influence
|
influenced future rocket designs
|
|
gptkbp:launch_date
|
frequent
|
|
gptkbp:launch_site
|
gptkb:Tanegashima_Space_Center
gptkb:railway_station
Japan Aerospace Exploration Agency (JAXA
|
|
gptkbp:launch_vehicle
|
gptkb:H-IIA_family
expendable launch vehicle
competitive launch costs
approximately 300,000 kg
|
|
gptkbp:launched
|
varies
multiple
|
|
gptkbp:legacy
|
successor to H-II rocket
|
|
gptkbp:manufacturer
|
gptkb:Mitsubishi_Heavy_Industries
|
|
gptkbp:marketed_as
|
used for commercial satellite launches
|
|
gptkbp:military_technology
|
limited military applications
|
|
gptkbp:mission
|
orbital insertion
communications satellites
|
|
gptkbp:notable_album
|
H-IIA 254 launch on 2006-02-24
|
|
gptkbp:number_of_stages
|
gptkb:LE-5_B
gptkb:LE-7_A
2
|
|
gptkbp:operational_area
|
2004 to 2014
|
|
gptkbp:operational_status
|
retired
|
|
gptkbp:partnerships
|
collaborated with various organizations
|
|
gptkbp:project
|
ongoing advancements in technology
|
|
gptkbp:propulsion
|
1,000 k N
|
|
gptkbp:public_perception
|
well-regarded in Japan
|
|
gptkbp:purpose
|
gptkb:spacecraft
|
|
gptkbp:reliability
|
proven
|
|
gptkbp:research
|
used for scientific missions
|
|
gptkbp:safety_record
|
excellent safety record
|
|
gptkbp:seating_capacity
|
gptkb:satellite
4 meters in diameter
4,000 kg to geostationary transfer orbit
|
|
gptkbp:setting
|
H-IIA 202 configuration
|
|
gptkbp:succeeded_by
|
high
|
|
gptkbp:technology
|
advanced rocket technology
|