MT-B
VENG S.A.
The MT-B is a bipropellant liquid rocket engine with a single regeneratively cooled thrust chamber, designed for the second stage of the Tronador TII-250 launch vehicle.
Key figurescomparable across the catalogue
- Thrust
- 41 974.48 N
- Specific impulse
- 330 s
Normalised to common units so this product can be compared with others in its category. The supplier's own wording is below.
As published by the supplier
- Uso
- Segunda etapa (óptima) o clúster de primera etapa
- Empuje en vac
- 4280 Kgf
- Propelentes
- LOX/RP1
- Impulso específico en vac
- 330 S
- Sistema de alimentación
- CICLO GENERADOR DE GASES
- Specific impulse
- 366 S
About
The MT-B is a bipropellant liquid rocket engine featuring a single, regeneratively cooled thrust chamber. It operates on an open-cycle, gas generator fed system. This engine was specifically developed as the propulsion system for the second stage of the Tronador TII-250 launch vehicle. The thrust chamber’s manufacturing process combined additive technology with electroforming. The manufacturer, VENG, has extensive experience in developing liquid rocket engines, including Hydrazine/Nitric Acid and LOx/Kerosene propellants, for various launcher prototypes such as TI, T4000, VEx 1A, Vex1B, and VEx5A. VENG is also the prime contractor for the design of the Tronador II series launcher engines, covering the entire propulsion value chain from requirements definition to design, simulation, manufacturing, testing, qualification, and integration.
Documentation
Need the full ICD, test reports or a specific revision? Ask the supplier directly.