Mitsubishi Heavy Industries

H-IIA 202

202

H-IIA 202
Retired

Overview

/01

H-IIA (H2A) is an active 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

202

Alias

N/A

Maiden Flight

August 29, 2001

Technical Specifications

/02
53 m

Length

4 m

Diameter

0 t

Launch Mass

2260 kN

Liftoff Thrust

10000 kg

LEO Capacity

4100 kg

GTO Capacity

Launch Record

/03
35

Total Launches

35

Successful

0

Failed

100.0%

Success Rate

0

Attempted Landings

0

Successful Landings

0

Failed Landings

0

Consecutive Successes

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