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Reference: 520/16
The outlets on the left and right hand sides offer the necessary cross-section and greatly reduce the forward thrust.This keeps the scale rear outlet while only discharging a small amount of the total exhaust gas.
Reference: 641/16
right / leftThis exhaust system is designed for the Air-Crane with turbine power system.
Reference: 429/16
Stainless steel exhaust manufactured specifically for the Bell 429
Reference: 791/16
Exhaust tubes for turbines are always designed for the specified model. It is important that no forward thrust emerges from the system. Should this still occur, the forward thrust produced is minimal.Turbine exhaust tubes are designed as exhaust-gas diffusers, i.e. opens wider towards the rear.
Reference: 770/16
On the BK 117 the forward thrust is eliminated by the scale division of the exhaust tube (enlarging of the cross-section) and exhausting up through the rotor disc.
Reference: 904/16
The shape and dimensions of the Hughes fuselages allow for the installation of a three outlet exhaust. The outlets on the left and right hand sides offer the necessary cross-section and greatly reduce the forward thrust. This keeps the scale rear outlet while only discharging a small amount of the total exhaust gas.
Reference: 350/17
When the turbine of a full-size helicopter is not running, the engine is protected with an exhaust cover which prevents foreign objects finding their way inside the turbine. This exhaust cover for model turbines is suitable for the Lama, Alouette III and any other machine with a 90 mm Ø exhaust pipe. Caution: it is essential to allow the exhaust pipes to...
Reference: 340/16
This exhaust system is designed for the Lama with turbine power system.
Reference: 434/16
On the AIRWOLF, Bell 230 and Bell 430 the forward thrust is eliminated by the scale division of the exhaust tube (enlarging of the cross-section) and exhausting up through the rotor disc.
Reference: 134/16
On the EC the forward thrust is eliminated by the scale division of the exhaust tube (enlarging of the cross-section) and exhausting up through the rotor disc.
