RS-2 Rocket Engine
VENG S.A.
Pressure-fed liquid rocket engine (LOX/RP-1) developed by VENG.
Technical specifications
- Thrust (sea level)
- 420 kgf
- Propellants
- LOX / RP-1
- Specific Impulse (sea level)
- 264 s
- Feed System
- Pressurized
About
The RS-2 is a pressure-fed liquid rocket engine developed by VENG using a LOX/RP-1 propellant combination.
Documentation
Need the full ICD, test reports or a specific revision? Ask the supplier directly.
