H-IIA/B First Stage Engine LE-7A
H-IIA/B First Stage Engine LE-7A
The LE-7A rocket engine is an improved version of the LE-7 engine, developed for the first stage of the H-II rocket and featuring a Staged Combustion Cycle.
To succeed in the highly competitive global satellite launch market, the LE-7A engine offers improved reliability, enhanced operability, and reduced costs compared to the LE-7 engine. The LE-7A engine is installed on the H-IIA and H-IIB rockets.
Main specifications
| Propellant | Liquid oxygen/ liquid hydrogen |
|---|---|
| Thrust (vacuum) | 112 ton |
| Isp (vacuum) | 440sec |
| Weight | 1,780kg |
| Length | 3,670mm |