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gptkbp:instance_of
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gptkb:Team_Rocket
|
|
gptkbp:collaboration
|
gptkb:Yes
|
|
gptkbp:control_system
|
Inertial navigation system
|
|
gptkbp:country_of_origin
|
gptkb:Japan
|
|
gptkbp:debut
|
Part of H-IIA program.
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|
gptkbp:design
|
15 years
JAXA launch team
|
|
gptkbp:diameter
|
4 meters
|
|
gptkbp:durability
|
No
|
|
gptkbp:engine_type
|
Liquid-fueled
|
|
gptkbp:first_flight
|
2019-11-17
2001-08-29
|
|
gptkbp:fuel_type
|
RP-1 and Liquid Oxygen
|
|
gptkbp:guidance_system
|
Inertial guidance
|
|
gptkbp:healthcare
|
Telemetry and command system
|
|
gptkbp:height
|
53 meters
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
H-IIA 294 rocket
|
|
gptkbp:launch_date
|
1-2 launches per year
2019-11-17
|
|
gptkbp:launch_event
|
Successful
|
|
gptkbp:launch_platform
|
gptkb:Japan_Aerospace_Exploration_Agency_(JAXA)
Satellite operations
Telemetry analysis
Remote control from ground station
|
|
gptkbp:launch_price
|
Approximately $90 million
|
|
gptkbp:launch_provider_type
|
Commercial launch service
|
|
gptkbp:launch_site
|
gptkb:Tanegashima_Space_Center
|
|
gptkbp:launch_vehicle
|
gptkb:H-IIA
Expendable launch vehicle
Standard configuration
|
|
gptkbp:launch_window
|
gptkb:N/_A
|
|
gptkbp:launched
|
gptkb:Launch_Complex_1
gptkb:1
6 months
|
|
gptkbp:manufacturer
|
gptkb:Mitsubishi_Heavy_Industries
|
|
gptkbp:mass
|
200,000 kg
|
|
gptkbp:mission
|
gptkb:DAICHI-2
gptkb:Earth_observation
|
|
gptkbp:mission_duration
|
gptkb:N/_A
|
|
gptkbp:mission_type
|
Commercial
|
|
gptkbp:notable_launches
|
gptkb:DAICHI-2
|
|
gptkbp:number_of_engines
|
gptkb:4
|
|
gptkbp:number_of_stages
|
gptkb:LE-5_B_engine
2
LE-7 A engine
|
|
gptkbp:operational_status
|
Retired
|
|
gptkbp:orbital_inclination
|
Geostationary orbit
|
|
gptkbp:payload_capacity
|
gptkb:Earth_observation
Vertical integration
4 meters in diameter
Multiple payload configurations
4,000 kg to geostationary transfer orbit
2,000 kg to low Earth orbit
Geostationary transfer orbit
|
|
gptkbp:payload_orbit
|
Geostationary orbit
|
|
gptkbp:payload_tracking
|
Satellite tracking system
|
|
gptkbp:production_status
|
Operational
|
|
gptkbp:propulsion
|
1,000 k N
|
|
gptkbp:safety_record
|
No major incidents
|
|
gptkbp:success
|
gptkb:1
|
|
gptkbp:supports
|
Standard ground support equipment
|
|
gptkbp:bfsParent
|
gptkb:Tanegashima_Space_Center
|
|
gptkbp:bfsLayer
|
4
|