MCA2 First-Stage Rocket Engine
VENG S.A.
First-stage liquid rocket engine (LOX/RP-1) developed by VENG for the Tronador II launch vehicle programme.
Technical specifications
- Stage
- First stage
- Thrust (sea level)
- 11,600 kgf
- Propellants
- LOX / RP-1
About
The MCA2 is a liquid-propellant (LOX/RP-1) rocket engine developed by VENG for the first stage of the Tronador II series of launch vehicles, as part of VENG’s full-cycle propulsion development work for CONAE covering design, simulation, manufacturing, testing, qualification and vehicle integration.
Documentation
Need the full ICD, test reports or a specific revision? Ask the supplier directly.
