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.
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Identity
- Aliases
- H-IIAH-2A
- Family Name
- H-IIA
- Full Name
- 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.
- Dimensions
- Diameter M
- 4
- Height M
- 53
- First Flight Year
- 2,001
- Last Flight Year
- 2,025
- Manufacturer
- Operator
- Parent Vehicle Family
- Propulsion Configurations
- Entries
- Nested value
- Nested value
- Rocket Specs
- Liftoff Mass Kg
- 289,000
- Payload Capacity Kg
- Gto
- 4,000
- Leo
- 10,000
- Reusability
- expendable
- Stages Count
- 2
Links
- Wikipedia Url
- https://en.wikipedia.org/wiki/H-IIA
Assets & Meta
- Creation Time
- July 13, 2026 at 10:03:00 UTC
- Updated Time
- July 29, 2026 at 15:38:16 UTC
- Image
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Other
- Search Name
- H-IIA Launch Vehicle H-IIA H-2A