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H-IIA (H-2A) is an expendable launch system operated by Mitsubishi Heavy Industries (MHI) for the Japan Aerospace Exploration Agency. The H-IIA is a derivative of the earlier H-II rocket, substantially redesigned to improve reliability and minimize costs. There have been four variants, with two in active service (as of 2021) for various purposes. A derivative design, the H-IIB, was developed in the 2000s and made its first flight in 2009.
Missions
50
Success Rate
98.0%
Successes
49
Failures
1
Success Streak
44
Partial Failures
0
Active 2006 to 2021
Payload to Orbit
LEO: 15,000 kg
GTO: 6,000 kg
Fairing
Diameter: 4.07m
Height: 12m
Stages
2
Strap-ons
4
Active 2002 to 2008
Rocket
Height: 53m
Payload to Orbit
GTO: 5,000 kg
Fairing
Diameter: 4.07m
Height: 12m
Stages
2
Strap-ons
4
Active 2005 to 2007
Rocket
Height: 53m
Payload to Orbit
GTO: 4,500 kg
Fairing
Diameter: 4.07m
Height: 12m
Stages
2
Strap-ons
2
Active 2001 to 2025
Price
$90.00 million
Rocket
Height: 53m
Payload to Orbit
LEO: 10,000 kg
GTO: 4,100 kg
Fairing
Diameter: 4.07m
Height: 12m
Stages
2
Strap-ons
2