About: H-IIA

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H-IIA (H2A) is an active expendable launch system operated by Mitsubishi Heavy Industries (MHI) for the Japan Aerospace Exploration Agency. The liquid-fueled H-IIA rockets have been used to launch satellites into geostationary orbit, to launch a lunar orbiting spacecraft, and to launch an interplanetary space probe to Venus. Launches occur at the Tanegashima Space Center.

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rdfs:comment	H-IIA (H2A) is an active expendable launch system operated by Mitsubishi Heavy Industries (MHI) for the Japan Aerospace Exploration Agency. The liquid-fueled H-IIA rockets have been used to launch satellites into geostationary orbit, to launch a lunar orbiting spacecraft, and to launch an interplanetary space probe to Venus. Launches occur at the Tanegashima Space Center.
foaf:name	H-IIA
foaf:depiction
country origin	Japan
diameter (μ)	4(xsd:double)
failed launches	1(xsd:integer)
height (μ)	53(xsd:double)
launch site	Tanegashima Yoshinobu
maiden flight	2001-08-29(xsd:dateTime) 2002-02-04(xsd:dateTime) 2005-02-26(xsd:dateTime) 2006-12-18(xsd:dateTime)
manufacturer	Alliant Techsystems Inc. Mitsubishi Heavy Industries, Ltd.
rocket function	dbpedia:Launch_vehicle
number of rocket stages	2(xsd:integer)
status	Active
successful launches	27(xsd:integer) 202(xsd:integer)
thumbnail	http://commons.wikimedia.org/wiki/Special:FilePath/H_IIA_No._F23_with_GPM_on_its_way_to_the_launchpad.jpg?width=300
total launches	28(xsd:integer) 202(xsd:integer)
is comparable of	Long March 7
is maiden flight rocket of	dbpedia:2005_in_spaceflight dbpedia:2006_in_spaceflight dbpedia:2001_in_spaceflight dbpedia:2002_in_spaceflight
is retired rocket of	dbpedia:2008_in_spaceflight dbpedia:2007_in_spaceflight

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