H-IIA 204
MHI
Details
Height
53 m
Diameter
4 m
GTO
6,000 kg
LEO
Unknown
Thrust at Liftoff
2,260 kN
Apogee
Unknown
Launch Cost
$90M
Maiden Flight
December 18, 2006
Description
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.