CV1 Micro Turbojet Engine
Micro Turbojet Engines / CV Series Turbojet Engines
Technical Specifications
| Max thrust | 25 kgf |
| Specific fuel consumption | ≤ 1.5 kg/kgf/h |
| Max outer diameter | 118 mm |
| Overall length | 300 mm |
| Weight (with accessories) | 7 kg |
| Operating altitude | 7,000 m |
| Starting time | ≤ 6 s (static to cruise) |
| Generator power output | ≥ 600 W |
| Service life | ≥ 30 h |
Features
| Integrated starter-generator | Yes |
| Fast reliable starting | ≤ 6 s wide envelope |
| Direct-combustion combustor | Centrifugal atomizing slinger |
| Application | Loitering munitions, small cruise missiles, target drones |
| Design philosophy | Smallest diameter in thrust class, low cost, military grade |
| Development status | Full design + prototype verified on ground test bench |
| Control | Full-authority digital engine control (FADEC) |
| Service life | ≥ 30 h |
| Starting time | ≤ 6 s (static to cruise) |
Introduction
The CV1 is a 25 kgf class micro turbojet engine independently developed by Harbin Jinshi Technology. It features an integrated starter-generator, direct-combustion centrifugal atomizing fuel slinger design, and full-authority digital engine control (FADEC). The engine delivers fast, reliable starts across a wide altitude envelope, built-in power generation, and military-grade reliability at a fraction of the cost of comparable products.
