|
gptkbp:instance_of
|
gptkb:rocket
|
|
gptkbp:bfsLayer
|
4
|
|
gptkbp:bfsParent
|
gptkb:JAXA
|
|
gptkbp:customer_support
|
gptkb:Japan_Aerospace_Exploration_Agency
|
|
gptkbp:debut_year
|
Part of H-IIA program
|
|
gptkbp:design
|
Mitsubishi Heavy Industries team
|
|
gptkbp:diameter
|
4 meters
|
|
gptkbp:engine
|
2
|
|
gptkbp:engine_type
|
Liquid rocket engine
|
|
gptkbp:events
|
Successful
|
|
gptkbp:first_flight
|
2006-02-24
2001-08-29
|
|
gptkbp:future_plans
|
No further missions planned.
|
|
gptkbp:guidance_system
|
Inertial guidance system
|
|
gptkbp:height
|
53 meters
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
H-IIA 291
|
|
gptkbp:launch_date
|
Approximately 30 minutes
2006-02-24
Conducted prior to launch
|
|
gptkbp:launch_site
|
gptkb:Tanegashima_Space_Center
gptkb:Mitsubishi_Heavy_Industries
Conducted by JAXA
|
|
gptkbp:launch_vehicle
|
gptkb:H-IIA
Retired
H-II family
H-IIA 202 configuration
Approximately 300 tons
|
|
gptkbp:launched
|
gptkb:musical
gptkb:Launch_Complex_1
Daytime
Operational
Several months
|
|
gptkbp:manufacturer
|
gptkb:Mitsubishi_Heavy_Industries
|
|
gptkbp:mission
|
gptkb:High
gptkb:DSN-1_satellite
Commercial
Geostationary orbit
Communications satellite deployment
|
|
gptkbp:mission_duration
|
Ongoing
|
|
gptkbp:number_of_stages
|
2
LE-7 A engine
H M7 A engine
|
|
gptkbp:orbital_inclination
|
Geostationary orbit inclination
|
|
gptkbp:propulsion
|
1,000 k N
|
|
gptkbp:reliability
|
gptkb:High
|
|
gptkbp:seating_capacity
|
Communications satellite
4 meters in diameter
4,000 kg to geostationary transfer orbit
Completed before launch
Successful deployment of payload
|
|
gptkbp:significant_event
|
First launch of the H-IIA 200 series
|
|
gptkbp:succeeded_by
|
gptkb:theorem
|
|
gptkbp:track
|
Telemetry and tracking system
|
|
gptkbp:type
|
Expendable launch vehicle
|