MES3K Second-Stage Rocket Engine
VENG S.A.
Pressure-fed second-stage rocket engine (MMH/NTO) developed by VENG for the Tronador II launch vehicle.
Technical specifications
- Stage
- Second stage
- Thrust (sea level)
- 2,975 kgf
- Propellants
- MMH / NTO
- Specific Impulse (vacuum)
- 317 s
- Feed System
- Pressurized
About
The MES3K is a pressure-fed, hypergolic (MMH/NTO) liquid rocket engine developed by VENG for the second stage of the Tronador II launch vehicle programme.
Documentation
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