|
gptkbp:instance_of
|
gptkb:rocket
|
|
gptkbp:bfsLayer
|
4
|
|
gptkbp:bfsParent
|
gptkb:Tanegashima_Space_Center
|
|
gptkbp:collaborations
|
NASA, ESA
|
|
gptkbp:debut_year
|
2001-2014
|
|
gptkbp:design
|
15 years
commercial satellite launch
|
|
gptkbp:developer
|
$1 billion
|
|
gptkbp:diameter
|
4 meters
|
|
gptkbp:engine
|
2
|
|
gptkbp:engine_type
|
gptkb:rocket
liquid-fueled
|
|
gptkbp:first_flight
|
2014-11-29
2001-08-29
|
|
gptkbp:fuel_type
|
RP-1 and Liquid Oxygen
|
|
gptkbp:guidance_system
|
inertial guidance
|
|
gptkbp:height
|
53 meters
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
H-IIA 210 rocket
|
|
gptkbp:inspiration
|
gptkb:H-II_rocket
|
|
gptkbp:launch_date
|
annual
2001-08-29
|
|
gptkbp:launch_site
|
gptkb:Tanegashima_Space_Center
gptkb:JAXA
gptkb:Mitsubishi_Heavy_Industries
|
|
gptkbp:launch_vehicle
|
gptkb:Launch_Complex_1
gptkb:H-IIA
expendable launch vehicle
|
|
gptkbp:launched
|
gptkb:30
gptkb:Tanegashima_Launch_Complex
varies
|
|
gptkbp:manufacturer
|
gptkb:Mitsubishi_Heavy_Industries
|
|
gptkbp:market
|
$90 million
|
|
gptkbp:mission
|
gptkb:spacecraft
high
|
|
gptkbp:notable_album
|
gptkb:H-IIA_202
|
|
gptkbp:number_of_stages
|
gptkb:LE-5_B
gptkb:LE-7_A
2
|
|
gptkbp:operational_area
|
gptkb:13
|
|
gptkbp:operational_status
|
retired
|
|
gptkbp:primary_user
|
gptkb:Japan_Aerospace_Exploration_Agency_(JAXA)
|
|
gptkbp:propulsion
|
1,000 k N
|
|
gptkbp:reliability
|
high
|
|
gptkbp:restoration
|
gptkb:none
|
|
gptkbp:seating_capacity
|
gptkb:Himawari_satellites
15 meters
4 meters
10,000 kg
4,000 kg
multiple payloads
|
|
gptkbp:setting
|
210
|
|
gptkbp:succeeded_by
|
98%
over 90%
|
|
gptkbp:successor
|
gptkb:H-IIB_rocket
|