LE-7
The original high-thrust staged-combustion first-stage engine developed for H-II.
Identity
- Domains
- spaceflight
- Identity Level
- model
- Kind
- liquid-rocket-engine
- Name
- LE-7
- Status
- retired
Details
- Description
- The original high-thrust staged-combustion first-stage engine developed for H-II.
- Family
- Propellants
- liquid hydrogenliquid oxygen
- Rocket Specs
- Cycle
- staged-combustion
- Vacuum Thrust Kn
- 1,079
Links
- Official Url
- https://global.jaxa.jp/projects/rockets/h2/
Assets & Meta
- Creation Time
- July 29, 2026 at 08:49:22 UTC
- Updated Time
- July 29, 2026 at 08:51:05 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-II Launch Vehicle official vehicle reference
- Accessed Date
- 2026-07-29
- Publisher
- Japan Aerospace Exploration Agency
- Title
- LE-7A