H-IIA Launch Vehicle
H-IIA was Japan's two-stage expendable flagship launch vehicle from 2001 through the final F50 flight in 2025. Four configurations—202, 2022, 2024, and 204—combined the liquid-hydrogen core with different solid-booster arrangements across 50 flights, 49 of which completed their planned launches.
Identity
- Aliases
- H-IIAH-2A
- Family Name
- H-IIA
- Full Name
- H-IIA Launch Vehicle
- Reusability
- expendable
- Slug
- h-iia-launch-vehicle
- Status
- retired
- Type
- rocket
Details
- Description
- H-IIA was Japan's two-stage expendable flagship launch vehicle from 2001 through the final F50 flight in 2025. Four configurations—202, 2022, 2024, and 204—combined the liquid-hydrogen core with different solid-booster arrangements across 50 flights, 49 of which completed their planned launches.
- Diameter M
- 4
- Engines
- Count
- 1
- Name
- LE-7A
- Placement
- core
- Count
- 1
- Name
- LE-5B
- Placement
- upper
- First Flight Year
- 2,001
- Height M
- 53
- Last Flight Year
- 2,025
- Liftoff Mass Kg
- 289,000
- Manufacturer Id
- jd78f0qx6y0pykq0j05qvmz7qn7kpnbp
- Operator Id
- jd78f0qx6y0pykq0j05qvmz7qn7kpnbp
- Parent Vehicle Family Id
- nd7jrtazwq037g6pf5wxg5prv18afrzt
- Payload Capacity Kg
- Gto
- 4,000
- Leo
- 10,000
- Stages Count
- 2
Links
- Wikipedia Url
- https://en.wikipedia.org/wiki/H-IIA
Assets & Meta
- Creation Time
- 7/13/2026, 10:03:00 AM
- Updated Time
- 7/14/2026, 5:19:32 PM