|
gptkbp:instance_of
|
gptkb:rocket
|
|
gptkbp:bfsLayer
|
4
|
|
gptkbp:bfsParent
|
gptkb:JAXA
gptkb:Japanese_Aerospace_Exploration_Agency
gptkb:Japanese_Aerospace_Exploration_Agency_(JAXA)
gptkb:Japan_Aerospace_Exploration_Agency_(JAXA)
|
|
gptkbp:data_type
|
shroud type
|
|
gptkbp:deployment
|
separation system
|
|
gptkbp:developer
|
$1 billion
|
|
gptkbp:diameter
|
4 meters
|
|
gptkbp:engine
|
staged combustion cycle
|
|
gptkbp:engine_type
|
gptkb:LE-7_A
|
|
gptkbp:events
|
successful
|
|
gptkbp:first_flight
|
2004-02-20
|
|
gptkbp:guidance_system
|
gptkb:hospital
|
|
gptkbp:height
|
53 meters
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
H-IIA 214
|
|
gptkbp:launch_date
|
approximately 2 per year
2004-08-29
2019-01-18
|
|
gptkbp:launch_site
|
gptkb:Tanegashima_Space_Center
conducted
100 personnel
Japan Aerospace Exploration Agency (JAXA
|
|
gptkbp:launch_vehicle
|
gptkb:Launch_Complex_1
gptkb:H-IIA
2
mobile launch platform
expendable launch vehicle
220,000 kg
|
|
gptkbp:launched
|
gptkb:14
6 months
daytime
standard configuration
|
|
gptkbp:manufacturer
|
gptkb:Mitsubishi_Heavy_Industries
|
|
gptkbp:market
|
$100 million
|
|
gptkbp:mission
|
gptkb:physicist
95%
commercial
successful
satellite deployment
direct injection to orbit
|
|
gptkbp:notable_album
|
gptkb:H-IIA_214_Flight_14
|
|
gptkbp:number_of_stages
|
2
1,000 k N
150 k N
|
|
gptkbp:operational_status
|
retired
|
|
gptkbp:operator
|
gptkb:Mitsubishi_Heavy_Industries
|
|
gptkbp:primary_user
|
gptkb:JAXA
commercial customers
|
|
gptkbp:release_region
|
gptkb:battle
|
|
gptkbp:reliability
|
high
|
|
gptkbp:seating_capacity
|
gptkb:DAICHI-2
10,000 kg
4,000 kg
vertical integration
4.0 meters
4,000 kg to geostationary transfer orbit
|
|
gptkbp:status
|
retired
|
|
gptkbp:succeeded_by
|
gptkb:theorem
100%
over 90%
|