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H3 Launch Vehicle

Japan’s H3 is a modular launch vehicle jointly developed by JAXA and Mitsubishi Heavy Industries, using two LE-9 first-stage engines, one LE-5B-3 second-stage engine, and selectable SRB-3 solid boosters.

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Identity

Aliases
H3H3 rocket
Family Name
H3 Launch Vehicle
Full Name
H3 Launch Vehicle
Status
active
Type
rocket

Details

Description
Japan’s H3 is a modular launch vehicle jointly developed by JAXA and Mitsubishi Heavy Industries, using two LE-9 first-stage engines, one LE-5B-3 second-stage engine, and selectable SRB-3 solid boosters.
First Flight Year
2,023
Propulsion Configurations
  • Entries
    • Count
      2
      Placement
      core
      Propulsion System
      Role
      main
      Stage
      first-stage
      Variant Notes
      MHI/JAXA specify two LE-9 first-stage engines.
    • Count
      1
      Placement
      upper
      Propulsion System
      Role
      upper-stage
      Stage
      second-stage
      Variant Notes
      MHI/JAXA specify one LE-5B-3 second-stage engine.
    Name
    H3-30S
    Notes
    MHI identifies H3-30S as the no-SRB-3 configuration with two LE-9 first-stage engines and one LE-5B-3 second-stage engine.
  • Entries
    • Count
      2
      Placement
      core
      Propulsion System
      Role
      main
      Stage
      first-stage
    • Count
      2
      Placement
      booster
      Propulsion System
      Role
      booster
      Stage
      first-stage
      Variant Notes
      MHI/JAXA specify two SRB-3 solid boosters.
    • Count
      1
      Placement
      upper
      Propulsion System
      Role
      upper-stage
      Stage
      second-stage
    Name
    H3-22
    Notes
    MHI identifies H3-22 as the two-SRB-3 configuration with two LE-9 first-stage engines and one LE-5B-3 second-stage engine.
  • Entries
    • Count
      2
      Placement
      core
      Propulsion System
      Role
      main
      Stage
      first-stage
    • Count
      4
      Placement
      booster
      Propulsion System
      Role
      booster
      Stage
      first-stage
      Variant Notes
      MHI/JAXA specify four SRB-3 solid boosters.
    • Count
      1
      Placement
      upper
      Propulsion System
      Role
      upper-stage
      Stage
      second-stage
    Name
    H3-24
    Notes
    MHI identifies H3-24 as the four-SRB-3 configuration with two LE-9 first-stage engines and one LE-5B-3 second-stage engine.
Rocket Specs
Stages Count
2

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Creation Time
August 13, 2026 at 22:51:40 UTC
Updated Time
August 20, 2026 at 05:01:08 UTC