Turbojet engine BPS TJ100P

Turbojet engine BPS WP120P


The BPS WP120 turbojet engine is a small, cost-effective 120 kg thrust turbojet engine independently . Structurally, itadopts a high-pressure fuel injection disk that can start quickly in a few seconds and can work nommally in coldhigh-altitude environments. .

At the same time, it has the ability to start at medium and high altitudes, which is anexcellent feature not available in current engines of the same level, making this type of engine the mainstreampower for small high-speed unmanned aerial vehicles in current military powers. .

For example, many Europeanloitering munitions use this type of engine. Our company mass-produces and supports high-speed drones for acertain enterprise and multiple high-speed target aircraft manufacturing enterprises, and 100% of all engine partsare manufactured domestically.

Technical parameters

  Metric units Imperial units
Max. thrust 1,200 N 269.76 Ibf
Fuel Consumption Rate 1.40 kg/daN.h 3.08 lb/daN.h
Thrust-to-Weight Ratio 8.75 8.75
Air Flow Rate 2 kg/s 4.41 lb/s
Maximum Speed 59000 r/min 59000 r/min

Typical applications

The ES-BPS-WP120 turbojet engine turbojet engines 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. The engines are also suitable for remote carriers.
BPS WP120 Application 03
BPS WP120 Application 02
BPS WP120 Application 01