Turbojet engine BPS TJ220
is more powerful turbojet engines than BPS TJ150 Turbojet engine With a maximum thrust of 2,200 N . While maintaining the same outer diameter and engine weight, they deliver 20% more thrust, making them ideal for various high-speed drone and aircraft. .
These engines are known for their excellent thrust-to-weight ratio and integrated starter-generator for reliable engine starts and onboard power supply. They are compact, lightweight, and fuel-efficient, Maximum Flight Altitude: 12500m,Minimum Operating Temperature: -45°C,Minimum Starting Temperature: -30°C,Maximum Operating Temperature: +60°C.
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Compact design
Excellent thrust/weight ratio
Lubrication with fuel and oil mixture
Electric start, possibility of in-flight restart
Quick windmill start under 7 secondsBuilt-in BLDC starter-generator including control unit (ECU) and inverter
Technical parameters
| Metric units | Imperial units | |
| Max. thrust | 2,200 N | 494.6 Ibf |
| Weight | 29.00 kg | 63.93 lb |
| Outer diameter | 320 mm | 12.59 in in |
| Lenght | 645 mm | 25.39 in |
| TBO | 30 hrs | 30 hrs |
Typical applications
BPS TJ220 small turbojet engine turbojet engine are ideal for a variety of applications, including missiles and target drones, where they are particularly valued for the saltwater recovery capability. Their compact design and low weight make them a perfect fit for high-speed UAV and UCAV systems. . .
