M150 Series Rocket Engine (A/B/C)
VENG S.A.
Family of pressure-fed small liquid rocket engines (variants A, B, C) developed by VENG.
Technical specifications
- Thrust (sea level), A/B
- 150 kgf
- Thrust (sea level), C
- 68 kgf
- Propellants
- N2O4 / mixed nitric acid
- Specific Impulse (sea level), A/B
- 220 s
- Specific Impulse (sea level), C
- 191 s
- Feed System
- Pressurized
About
The M150 series comprises three pressure-fed liquid rocket engine variants (A, B and C) developed by VENG using an N2O4/mixed nitric-acid propellant combination, used in Argentina’s experimental and launch vehicle programme.
Documentation
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