H-IIA 204 is an expendable launch vehicle built by Mitsubishi Heavy Industries. It stands 53.0 m tall, first flew on 18 December 2006. It has flown 5 times with 5 successes, a success rate of 100.0%. It has nothing on the Launch Library 2 schedule right now.
Specification
Vehicle spec sheet
OPS-12/SPEC
ON FILE
Height53.0 m
Diameter4.0 m
Payload to LEONOT ON FILE
Payload to GTO6,000 kg
Maiden flight18 December 2006
ReusableNo, expendable
Launch cost$90M
StatusRETIRED
As listed by Launch Library 2. The cost is Launch Library’s figure, not a quoted price. Figures for rockets outside the sixty most-flown were last read on 2026-11-05.
Flight record
Reliability
OPS-12/STAT
ON RECORD
Total flights5
Successful5
Failed0
Success rate100.0%
Landing attempts0
Landing successN/A
Scheduled0
Variant204
About H-IIA
H-IIA (H2A) was an 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 Akatsuki, which studied the planet Venus. Launches occur at the Tanegashima Space Center.
From NASA's public image library and Wikimedia Commons. Each photo shows the credit its licence asks for and links back to where it came from.
Homiliarium de Tempore. - btv1b525256340 (204 of 450)·S. Leo Magnus. Auteur du texte AMBROSIUS MEDIOLANENSIS ep. (s.). Auteur du texte AUGUSTINUS HIPPONENSIS ep. (s.). Auteur du texte BEDA VENERABILIS (s.). Auteur du texte CAESARIUS ARELATENSIS ep. (s.). Auteur du texte EPIPHANIUS LATINUS. Auteur du texte EUSEBIUS (s.) Cremonensis, discipulus s. Hieronymi. Auteur du texte HAYMO AUTISSIODORENSIS. Auteur du texte HIERONYMUS (s.). Auteur du texte JOHANNES CHRYSOSTOMUS (s.). Auteur du texte LEO Magnus I (s.), papa. Auteur du texte MAXIMUS TAURINENSIS ep. (s.). Auteur du texte ORIGENES. Auteur du texte ORIGENES (Pseudo-). Auteur du texte PETRUS CHRYSOLOGUS (s.), Ravennatensis ep. Auteur du texte RABANUS MAURUS. Auteur du texte · public domain·Wikimedia Commons ↗
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Common questions
How many times has H-IIA 204 flown?
5 times, with 5 successes and 0 failures.
What is H-IIA 204's success rate?
100.0%. That's 5 successful flights out of 5 attempts.
How much can H-IIA 204 lift to orbit?
Launch Library 2 lists H-IIA 204 at no figure to low Earth orbit and 6,000 kg to geostationary transfer orbit.
Is H-IIA 204 reusable?
No. Launch Library 2 lists H-IIA 204 as expendable, so no stage is recovered to fly again.
