Ιαπωνικός πυραυλοφορέας δορυφόρων H-IIA

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Ιαπωνικός πυραυλοφορέας δορυφόρων H-IIA

Name Ιαπωνικός πυραυλοφορέας δορυφόρων H-IIA
Description Ξενάγηση στη βάση εκτόξευσης και τον Ιαπωνικό πυραυλο H-IIA που χρησιμοποιείται για να τοποθετηθούν σε τροχιά τηλεπικοινωνιακοί και DTH δορυφόροι


Japanese Main Large-scale Launch Vehicle
is Japan's primary large-scale launch vehicle equipped with high-performance engines with liquid oxygen and hydrogen as propellants. Its operability is highly flexible as it can launch payloads (mainly satellites) of various weights, and inject them into different orbits in the space. Therefore, it is categorized one of the world top-level launch vehicles both in technology and launch costs.
JAXA (NASDA at that time) successfully launched the H-IIA F1 in Aug. 2001, and full-scale operations for launching practical satellites started with the H-IIA F3. However, the H-IIA F6 failed in Nov. 2003. After a thorough investigation, the cause of the failure was found to be the sold rocket booster (SRB-A).

JAXA performed numerous experiments and tests to modify the troubled parts, including the shape of the injector. H-IIA F7 launched in 26 Feb. 2005 and could carry a satellite into the scheduled orbit.
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