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LE-5
The original Japanese cryogenic upper-stage engine flown by the retired H-I launch vehicle.
Identity
Domains
spaceflight
Identity Level
model
Kind
liquid-rocket-engine
Name
LE-5
Status
retired
Details
Description
The original Japanese cryogenic upper-stage engine flown by the retired H-I launch vehicle.
Family
Family
Propellants
liquid hydrogen
liquid oxygen
Rocket Specs
Cycle
gas-generator
Restartable
Yes
Vacuum Specific Impulse S
450
Vacuum Thrust Kn
103
Links
Official Url
https://global.jaxa.jp/projects/rockets/h1/index.html
Assets & Meta
Creation Time
July 29, 2026 at 08:48:30 UTC
Updated Time
July 29, 2026 at 08:50:23 UTC
Other
Sources
Accessed Date
2026-07-29
Note
Supports the legacy vehicle installation and the narrow canonical identity used for migration.
Publisher
Official vehicle or program source
Title
H-I Launch Vehicle official vehicle reference
Url
https://global.jaxa.jp/projects/rockets/h1/index.html
Accessed Date
2026-07-29
Publisher
Japan Aerospace Exploration Agency
Title
LE-5B
Url
https://www.rocket.jaxa.jp/rocket/engine/le5b/index.html
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