Pitot-Static Systems

 

PITOT TUBE - LUN 1157

This tube is designed for reliable sensing of total air pressure up to transonic speeds. The outlet is located at the top of the support. The tube consists of a streamlined brass body, the outer surface of which is nickel plated and polished. A heater element with automatic maximum temperature control can be installed inside the tube to eliminate the risk of icing during flights in bad weather conditions. This product can be fully customized. Don't hesitate to contact us with your inquiry.

 

 

PITOT-STATIC TUBE - LUN 1152

This tube is designed for reliable sensing of total and static air pressure at subsonic speeds (up to 380 kts / 700 km/h). The outlets with marking are located at the rear end of the tube. The tube consists of a streamlined brass body, the outer surface of which is painted. A heater element can be installed inside the tube to eliminate the risk of icing during flights in bad weather conditions. It is a proven solution for aircrafts, helicopters and UAV systems. This product can be fully customized. Don't hesitate to contact us with your inquiry.

 

 

PITOT-STATIC TUBE - LUN 1150

This tube is designed for reliable sensing of total and static air pressure up to transonic and supersonic speeds. The outlets with marking are located at the rear end of the tube. The tube consists of a streamlined brass body, the outer surface of which is nickel plated and polished. There is a heater element inside of the tube to eliminate the risk of icing during flights in bad weather conditions. This product can be fully customized. Don't hesitate to contact us with your inquiry.

 


PITOT-STATIC TUBE - LUN 1153

This tube is designed for reliable sensing of total and static air pressure up to transonic and supersonic speeds. The outlets with marking are located at the rear end of the tube. The tube consists of a streamlined brass body, the outer surface of which is nickel plated and polished. There is a heater element inside of the tube to eliminate the risk of icing during flights in bad weather conditions. The difference between LUN 1150 and LUN 1153 is two rows of scanning apertures and a dual conduit of static pressure. This allows connection of several devices to a static system. This product can be fully customized. Don't hesitate to contact us with your inquiry.

 

 

PITOT-STATIC TUBE - LUN 1162

This tube is designed for reliable sensing of total and static air pressure up to transonic and supersonic speeds. The outlets with marking are located at the rear end of the tube. The tube consists of a streamlined brass body, the outer surface of which is nickel plated and polished. There is a heater element inside of the tube to eliminate the risk of icing during flights in bad weather conditions. The tube has two rows of scanning apertures and a dual conduit of static pressure. This allows connection of several devices to a static system. This product can be fully customized. Don't hesitate to contact us with your inquiry.

 

 

STATIC PRESSURE SENSOR - LUN 1155

This sensor is designed for reliable sensing of static air pressure (single output). The outer surface is nickel plated and polished, the outlets are located at the rear end of the sensor. A heater element can be installed inside the sensor to eliminate the risk of icing during flights in bad weather conditions. This product can be fully customized. Don't hesitate to contact us with your inquiry.

 

 

STATIC PRESSURE SENSOR - LUN 1156

This sensor is designed for reliable sensing of static air pressure (double output). The outer surface is painted, the outlets are located at the rear end of the sensor. A heater element can be installed inside the sensor to eliminate the risk of icing during flights in bad weather conditions. This product can be fully customized. Don't hesitate to contact us with your inquiry.

 

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