Mitsubishi Heavy Industries

H-IIA 204

204

H-IIA 204
Retired

Overview

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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.

Manufacturer

Mitsubishi Heavy Industries

Variant

204

Alias

N/A

Maiden Flight

December 18, 2006

Technical Specifications

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53 m

Length

4 m

Diameter

0 t

Launch Mass

2260 kN

Liftoff Thrust

LEO Capacity

6000 kg

GTO Capacity

Launch Record

/03
5

Total Launches

5

Successful

0

Failed

100.0%

Success Rate

0

Attempted Landings

0

Successful Landings

0

Failed Landings

0

Consecutive Successes

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