H-IIA 210

GPTKB entity

Predicate	Object
gptkbp:instance_of	gptkb:aircraft 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:diameter	4 meters
gptkbp:engine_type	gptkb:LE-7_A
gptkbp:first_flight	2004-08-29 2001-08-29 2009-03-12
gptkbp:fuel_type	Liquid hydrogen and liquid oxygen
gptkbp:height	53 meters
https://www.w3.org/2000/01/rdf-schema#label	H-IIA 210
gptkbp:launch_date	2004-02-21
gptkbp:launch_site	gptkb:Tanegashima_Space_Center
gptkbp:launch_vehicle	2 200,000 kg
gptkbp:manufacturer	gptkb:Mitsubishi_Heavy_Industries
gptkbp:number_of_stages	2
gptkbp:operator	gptkb:Mitsubishi_Heavy_Industries
gptkbp:orbital_inclination	Geostationary orbit
gptkbp:propulsion	1,000 k N
gptkbp:reliability	100%
gptkbp:seating_capacity	10,000 kg 4,000 kg 4,000 kg to geostationary transfer orbit Various satellites
gptkbp:setting	gptkb:H-IIA_202
gptkbp:strategic_importance	gptkb:0
gptkbp:succeeded_by	gptkb:10 over 90%