High Thrust-to-Weight Ratio Turbojet Engine with High-Altitude Rapid Start Capability and 100~300kgf Range for Missiles
Product Details
| Thrust Range: | 100~300kgf | Power Output: | 400~1000kW |
|---|---|---|---|
| Turbofan Thrust: | 300~1000kgf | Thrust-to-Weight Ratio: | 10 |
| Specific Fuel Consumption: | 1.4~1.1kg/(kgf·h) | Diameter: | 156~350mm |
| Length: | 397~855mm | Weight: | 4.5~54kg |
| Max Take-off Altitude: | 5000~8000m | Max Flight Altitude: | 8000~16000m |
| Max Flight Speed: | 0.8~0.95Ma | Customization Lead Time: | 3~5 Months |
Product Description
- Comprehensive product range (100~300kgf turbojet engines, 400~1000kW turbogenerator engines, and 300~1000kg turbofan engines)
- Cutting-edge performance (thrust-to-weight ratio of 10 and high-altitude rapid start capability)
- Exceptional stability and reliability (fully validated through 100 test prototypes, high-altitude tests, and flight tests)
- High production capacity (annual output of thousands of units)
- Excellent after-sales service (professional after-sales support team)
- Strong product customization capabilities (customized products deliverable within 3 to 5 months)
- 100~300kgf turbojet engines for missiles (gun start/motor start options)
- 300~600kW high-efficiency turbogenerator hybrid engines
- 500~800kgf long-endurance turbofan engines
| Parameter/Model | LJ40P | LJ80P | LJ120P | LJ160P |
|---|---|---|---|---|
| Power Generation Output (kW) | / | 1.6 | 2 | 2 |
| Specific Fuel Consumption (kg/(kgf·h)) | 1.4 | 1.3 | 1.2 | 1.18 |
| Diameter * Length (mm*mm) | 156*397 | 200*482 | 239*617 | 275*648 |
| Weight (kg) | 4.5 | 7.8 | 13.5 | 20.5 |
| Maximum Take-off Altitude (m) | 5000 | 8000 | 8000 | 8000 |
| Maximum Flight Altitude (m) | 8000 | 12000 | 12000 | 12000 |
| Maximum Flight Speed (Ma) | 0.8 | 0.95 | 0.95 | 0.95 |
| Parameter/Model | LJ200P | LJ260P | LJ300P |
|---|---|---|---|
| Power Generation Output (kW) | 2 | 2.5 | 2.5 |
| Specific Fuel Consumption (kg/(kgf·h)) | 1.15 | 1.12 | 1.1 |
| Diameter * Length (mm*mm) | 303*726 | 335*765 | 350*855 |
| Weight (kg) | 30 | 43 | 54 |
| Maximum Take-off Altitude (m) | 8000 | 8000 | 8000 |
| Maximum Flight Altitude (m) | 16000 | 16000 | 16000 |
| Maximum Flight Speed (Ma) | 0.95 | 0.95 | 0.95 |
Product Highlights
Turbojet engines with 10:1 thrust-to-weight ratio, high-altitude rapid start, and proven reliability. Customizable options (100-300kgf) with fast 3-5 month delivery. Annual capacity of thousands ensures supply.
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