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gptkbp:instance_of
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gptkb:rocket
|
|
gptkbp:bfsLayer
|
4
|
|
gptkbp:bfsParent
|
gptkb:JAXA
|
|
gptkbp:controls
|
Digital control system
|
|
gptkbp:country
|
gptkb:Japan
|
|
gptkbp:debut_year
|
gptkb:H-IIA_254
gptkb:H-IIA_252
Part of H-IIA program
|
|
gptkbp:diameter
|
4 meters
|
|
gptkbp:engine
|
2
|
|
gptkbp:engine_type
|
Liquid-fueled
|
|
gptkbp:events
|
Successful
|
|
gptkbp:first_flight
|
2001-08-29
|
|
gptkbp:guidance_system
|
Inertial navigation system
|
|
gptkbp:height
|
53 meters
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
H-IIA 253
|
|
gptkbp:launch_date
|
Several per year
2019-01-18
|
|
gptkbp:launch_site
|
gptkb:Tanegashima_Space_Center
gptkb:JAXA
|
|
gptkbp:launch_vehicle
|
gptkb:H-IIA
H-II family
|
|
gptkbp:launched
|
gptkb:Launch_Complex_1
253
Daytime
50+
|
|
gptkbp:manufacturer
|
gptkb:Mitsubishi_Heavy_Industries
|
|
gptkbp:market
|
Approximately $90 million
|
|
gptkbp:mission
|
Commercial
95%
Communications satellite deployment
|
|
gptkbp:number_of_stages
|
2
LE-7 A engine
H M7 A engine
|
|
gptkbp:operational_status
|
Active
|
|
gptkbp:orbital_inclination
|
Geostationary orbit
|
|
gptkbp:propulsion
|
1,000 k N
|
|
gptkbp:reliability
|
gptkb:High
|
|
gptkbp:seating_capacity
|
gptkb:DSN-1_satellite
4 meters
Geostationary orbit
4,000 kg
4,000 kg to geostationary transfer orbit
|
|
gptkbp:succeeded_by
|
gptkb:theorem
|
|
gptkbp:tour
|
Two-stage
|