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Retired

H-IIA

H-IIA 204

🏭 Mitsubishi Heavy Industries🌐 Japanese📖 Wikipedia
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.

📊 Specifications

📏Height
53 m
⭕Diameter
4 m
⚖️Launch Mass
445 kg
🛰️LEO Capacity
—
🌍GTO Capacity
6,000 kg
🗓️Maiden Flight
Dec 18, 2006
🚀Total Launches
5
✅Success Rate
100%
♻️Reusable
Expendable
🏭Manufacturer
Mitsubishi Heavy Industries
🌐Country
Japanese
📋Status
Retired

📷 Photo Gallery

H-IIA 204 photo 1

🛰️ Launch History