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Retired

H-IIA

H-IIA 202

🏭 Mitsubishi Heavy Industries🌐 Japanese📖 Wikipedia
H-IIA

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.

10.0 t
LEO Capacity
53 m
Height
35
Total Launches
100.0%
Success Rate

📷 Photo Gallery

H-IIA 202 photo 1

📊 Specifications

📏Height
53 m
⭕Diameter
4 m
⚖️Launch Mass
285 kg
🛰️LEO Capacity
10,000 kg
🌍GTO Capacity
4,100 kg
🗓️Maiden Flight
Aug 29, 2001
🚀Total Launches
35
✅Success Rate
100%
♻️Reusable
Expendable
🏭Manufacturer
Mitsubishi Heavy Industries
🌐Country
Japanese
📋Status
Retired