H-IIB (H2B) is a launch system used to launch H-II Transfer Vehicles towards the International Space Station. H2B rockets are launched from the Tanegashima Space Center in Japan. H-IIB is built by Mitsubishi Heavy Industries. H-IIB is derived from the original H-II and the H-IIA that underwent modifications to reduce costs and increase
reliability and to increase its payload capacity for the heavy HTV. The H-IIB was designed to adopt methods and components that have already been verified by flights on the H-IIA, so that manufacturing the new launch vehicle would be more cost-effective, with less risk, in a shorter period of time.
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Showing posts with label H-IIA. Show all posts
Showing posts with label H-IIA. Show all posts
Saturday, 10 October 2015
H-IIA
H-IIA (H2A) is an launch system operated by Mitsubishi Heavy Industries (MHI) for the Japan Aerospace Exploration Agency. 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. All
Launches occur at the Tanegashima Space Center . It first flew in 2001 and has been launched 28 times. Current Launches are operated by MHI only as JAXA handed the Launch System over in 2007.
Launches occur at the Tanegashima Space Center . It first flew in 2001 and has been launched 28 times. Current Launches are operated by MHI only as JAXA handed the Launch System over in 2007.
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