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LE-5B-2

Retired JAXA LE-5B-2 expander-bleed cryogenic upper-stage engine, a vibration-reduced LE-5B update for later H-IIA/H-IIB-era missions. JAXA documents multiple in-space ignitions plus idle-mode low-thrust operation for controlled post-mission stage disposal and throttling for higher orbital-insertion accuracy; the canonical H-IIB upper-stage installation and LE-5B derivative lineage are preserved.

Identity

Domains
spaceflight
Identity Level
variant
Kind
liquid-rocket-engine
Name
LE-5B-2
Status
retired

Details

Description
Retired JAXA LE-5B-2 expander-bleed cryogenic upper-stage engine, a vibration-reduced LE-5B update for later H-IIA/H-IIB-era missions. JAXA documents multiple in-space ignitions plus idle-mode low-thrust operation for controlled post-mission stage disposal and throttling for higher orbital-insertion accuracy; the canonical H-IIB upper-stage installation and LE-5B derivative lineage are preserved.
Family
Lineage
  • Note
    JAXA documents LE-5B-2 as a design update of LE-5B to reduce combustion-pressure oscillation.
    Related Propulsion System
    Relationship
    direct-derivative-of
    Sources
Propellants
liquid hydrogenliquid oxygen
Rocket Specs
Cycle
expander-bleed
Restartable
Yes
Vacuum Thrust Kn
137

Links

Assets & Meta

Creation Time
July 29, 2026 at 08:48:42 UTC
Updated Time
August 15, 2026 at 08:13:54 UTC

Other

Sources