CV2 Micro Turbojet Engine
Micro Turbojet Engines / CV Series Turbojet Engines
Technical Specifications
| Max thrust | 125 kgf |
| Specific fuel consumption | ≤ 1.35 kg/kgf/h |
| Max outer diameter | 230 mm |
| Overall length | 570 mm |
| Weight (with accessories) | 20 kg |
| Operating altitude | 11,000 m |
| Starting time | ≤ 10 s (static to cruise) |
| Generator power output | ≥ 2,000 W |
| Service life | ≥ 30 h |
Features
| Integrated starter-generator | Yes |
| High-altitude wide-envelope start | Fast and reliable |
| Smallest diameter in class | Advanced small-radial-ratio integrated diffuser |
| Direct-combustion combustor | Centrifugal atomizing slinger |
| Application | Cruise missiles, fast target drones, large UAVs |
| Control | Full-authority digital engine control (FADEC) |
| Development status | Full design + prototype verified on ground test bench |
| Service life | ≥ 30 h |
Introduction
The CV2 is a 125 kgf class micro turbojet engine with a fully integrated generator and high-altitude wide-envelope fast starting capability. Its advanced small-radial-ratio integrated diffuser achieves the smallest outer diameter among engines of the same thrust class, minimizing vehicle frontal drag. Its military applications include loitering munitions, cruise missiles and high-speed target drones.
