LE-5B
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The LE-5B rocket engine, developed for the second stage of the H-II rocket, is the improved model of LE-5A engine. It is the first rocket engine in the world which uses the hydrogen used for the cooling of the thrust chamber as the turbine gas.
| Propellant | Liquid oxygen/liquid hydrogen |
|---|---|
| Thrust (vacuum) | 14 ton |
| Isp(vacuum) | 449sec |
| Weight | 285kg |
| Length | 2,765mm |
Business contact: Aerospace Systems -
