|
gptkbp:instance_of
|
gptkb:Team_Rocket
|
|
gptkbp:configuration
|
205
|
|
gptkbp:control_system
|
gptkb:navigation_system
|
|
gptkbp:debut
|
launched various satellites
|
|
gptkbp:diameter
|
4 meters
|
|
gptkbp:elevation
|
4 meters
53 meters
approximately 300,000 kg
|
|
gptkbp:engine_configuration
|
staged combustion cycle
|
|
gptkbp:engine_type
|
gptkb:LE-7_A
|
|
gptkbp:first_flight
|
gptkb:2001
|
|
gptkbp:guidance_system
|
gptkb:GPS
|
|
gptkbp:height
|
53 meters
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
H-IIA 205
|
|
gptkbp:launch_date
|
several per year
2019-01-17
|
|
gptkbp:launch_event
|
high success rate
|
|
gptkbp:launch_platform
|
gptkb:JAXA
gptkb:ground
gptkb:missions
|
|
gptkbp:launch_price
|
approximately $90 million
|
|
gptkbp:launch_site
|
gptkb:Tanegashima_Space_Center
|
|
gptkbp:launch_vehicle
|
gptkb:H-IIA
two-stage
satellite deployment
expendable
varied by configuration
H-II series
over 40 launches
successful satellite placements
|
|
gptkbp:launch_window
|
varies by mission
|
|
gptkbp:launched
|
multiple
automated
several months
|
|
gptkbp:manufacturer
|
gptkb:Mitsubishi_Heavy_Industries
|
|
gptkbp:mission_duration
|
gptkb:unknown
varies by payload
|
|
gptkbp:mission_type
|
commercial
orbital launch
|
|
gptkbp:notable_launches
|
gptkb:Hayabusa_mission
|
|
gptkbp:number_of_engines
|
2
|
|
gptkbp:number_of_stages
|
2
|
|
gptkbp:operational_status
|
active
|
|
gptkbp:operator
|
gptkb:Mitsubishi_Heavy_Industries
|
|
gptkbp:orbit_type
|
geostationary transfer orbit
|
|
gptkbp:payload_capacity
|
4 meters in diameter
in orbit
pre-launch processing
4,000 kg to geostationary transfer orbit
commercial and scientific
DSN-1
|
|
gptkbp:production_status
|
operational
|
|
gptkbp:propulsion
|
liquid hydrogen and liquid oxygen
1,000 k N
|
|
gptkbp:recovery_method
|
gptkb:none
|
|
gptkbp:release_country
|
yes
|
|
gptkbp:reliability
|
high
|
|
gptkbp:success
|
gptkb:true
|
|
gptkbp:success_rate
|
over 90%
|
|
gptkbp:bfsParent
|
gptkb:Team_Rocket
|
|
gptkbp:bfsLayer
|
3
|