The PBS TJ80-120 is a small sub-sonic turbojet engine produced by a Czech turbine engine manufacturer PBS Velká Bíteš. The engine has been developed for unmanned aerial vehicles, including target drones, remote carriers, unmanned combat systems and disposable applications with weight ranging from 330-551 lb (150-250 kg).[1][2] The PBS TJ80-120 has the best thrust-to-weight ratio among gas turbine engines with thrust more than 1,150 N.[3] With a thrust 269 lbf (1,200 N) and weight 28.21 lb (12.8 kg) including the accessories, the thrust-to-weight ratio is currently 9.53.

The topic of this article may not meet Wikipedia's notability guidelines for products and services. (September 2022)

Design

The PBS TJ80-120 is a small single-shaft turbojet engine with a built-in brushless starter generator including the ECU. The engine is capable of ground and in-flight restart under 7 seconds and a windmill starting. The engine offers a possibility of salt water recovery.[1]

Specifications

General characteristics

• Type: Turbojet
• Length: 25.04 in (636 mm)
• Outer diameter: 10.71 in (272 mm)
• Weight: 28.21 lb (12.8 kg)
• Thrust-to-Weight ratio: 9.53

Performance

• Thrust: 202-269 lbf (900-1,200 N)
• Power Supply: 28 V DC
• Electrical Power Output: 650-2,250 W

References