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KM-V2c

JAXA's KM-V2c is the exact Enhanced Epsilon third-stage solid motor, partially modified from the M-V KM-V2. The current Epsilon User's Manual lists 2.3 m length, 1.4 m diameter, 3.3 t stage weight, 2.5 t propellant, 99.8 kN thrust, 90 s burn time, and 301 s specific impulse. This record uses active for current JAXA documentation of the Enhanced Epsilon configuration and keeps KM-V2c distinct from the M-V KM-V2 and the successor Epsilon S third-stage design.

Identity

Aliases
KM-V2cEpsilon KM-V2c
Domains
spaceflight
Identity Level
model
Kind
solid-rocket-motor
Name
KM-V2c
Status
active

Details

Description
JAXA's KM-V2c is the exact Enhanced Epsilon third-stage solid motor, partially modified from the M-V KM-V2. The current Epsilon User's Manual lists 2.3 m length, 1.4 m diameter, 3.3 t stage weight, 2.5 t propellant, 99.8 kN thrust, 90 s burn time, and 301 s specific impulse. This record uses active for current JAXA documentation of the Enhanced Epsilon configuration and keeps KM-V2c distinct from the M-V KM-V2 and the successor Epsilon S third-stage design.
Length M
2.3
Propellants
solid HTPB composite
Rocket Specs
Burn Time S
90
Vacuum Specific Impulse S
301
Vacuum Thrust Kn
99.8

Links

Assets & Meta

Creation Time
August 1, 2026 at 16:32:33 UTC
Updated Time
August 21, 2026 at 00:21:11 UTC

Other

Diameter M
1.4
Sources
  • Accessed Date
    2026-08-01
    Note
    JAXA identifies KM-V2c as the exact Epsilon third-stage motor, describes its partial modification from KM-V2, and lists its solid HTPB propellant.
    Publisher
    Japan Aerospace Exploration Agency
    Title
    Epsilon User's Manual
  • Accessed Date
    2026-08-01
    Note
    JAXA documents the Epsilon third-stage inheritance from M-V propulsion technology while preserving the exact KM-V2c boundary.
    Publisher
    Japan Aerospace Exploration Agency
    Title
    Epsilon Technology: A Link to the Future
  • Accessed Date
    2026-08-20
    Note
    JAXA's current Epsilon User's Manual identifies KM-V2c as the third stage of Enhanced Epsilon and lists 2.3 m length, 1.4 m diameter, 3.3 t stage weight, 2.5 t propellant, 99.8 kN thrust, 90 s burn time, and 301 s specific impulse.
    Publisher
    Japan Aerospace Exploration Agency
    Title
    Epsilon User's Manual
  • Accessed Date
    2026-08-20
    Note
    JAXA's Space Transportation Technology Directorate documents the Enhanced Epsilon propulsion architecture and distinguishes its inherited second- and third-stage technology from the successor Epsilon S configuration.
    Publisher
    Japan Aerospace Exploration Agency Space Transportation Technology Directorate
    Title
    Epsilon