MT-B Bipropellant Rocket Engine
VENG S.A.
Single-chamber bipropellant (LOX/RP-1) liquid rocket engine in development by VENG, suited to a second stage or clustered first-stage application.
Technical specifications
- Thrust (vacuum)
- 4,280 kgf
- Propellants
- LOX / RP-1
- Specific Impulse (vacuum)
- 330 s
- Feed System
- Open-cycle gas generator
- Application
- Second stage or clustered first-stage
About
The MT-B is a single-chamber bipropellant (LOX/RP-1) liquid rocket engine in development by VENG using an open-cycle gas-generator feed system. It is optimal for use as a second-stage engine or in a clustered first-stage configuration for the Tronador II launch vehicle family.
Documentation
Need the full ICD, test reports or a specific revision? Ask the supplier directly.
