H-IIA 202
H-IIA 202 was the standard configuration with two SRB-A solid rocket boosters and no small strap-on boosters. It was used by 35 of the program's 50 flight vehicles from the 2001 test flight through the final F50 mission in 2025.
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Identity
- Aliases
- H2A202H-IIA-202
- Family Name
- H-IIA
- Full Name
- H-IIA 202
- Status
- retired
- Type
- rocket
- Variant Name
- 202
Details
- Description
- H-IIA 202 was the standard configuration with two SRB-A solid rocket boosters and no small strap-on boosters. It was used by 35 of the program's 50 flight vehicles from the 2001 test flight through the final F50 mission in 2025.
- First Flight Year
- 2,001
- Last Flight Year
- 2,025
- Manufacturer
- Operator
- Parent Vehicle Family
- Propulsion Configurations
- Entries
- Count
- 1
- Placement
- core
- Propulsion System
- Role
- main
- Stage
- first-stage
- Variant Notes
- One exact LE-7A liquid engine on the H-IIA 202 first stage.
- Count
- 2
- Placement
- booster
- Propulsion System
- Role
- booster
- Stage
- first-stage
- Variant Notes
- Two exact SRB-A solid rocket boosters on the standard H-IIA 202 configuration.
- Count
- 1
- Placement
- upper
- Propulsion System
- Role
- upper-stage
- Stage
- second-stage
- Variant Notes
- One exact LE-5B engine on the H-IIA 202 second stage.
- Name
- H-IIA 202
- Notes
- Exact standard H2A202 propulsion stack: one LE-7A first-stage engine, two SRB-A strap-on solid boosters, and one LE-5B second-stage engine. H-IIA 204 and other H-IIA forms remain separate variants.
- Rocket Specs
- Reusability
- expendable
- Stages Count
- 2
- Strap On Boosters Count
- 2
Links
- Official Url
- https://global.jaxa.jp/projects/rockets/h2a/
Assets & Meta
- Creation Time
- July 13, 2026 at 09:57:20 UTC
- Updated Time
- August 1, 2026 at 10:47:12 UTC
- Image
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