

No brand
Référence: 2017 E
Référence: 34/30
Tail rotor bladesSpecification 8.0 mm blade root8.7 g approx.29 mm blade chord5.0 mm profile thicknesssymmetrical130 mm longbalanced1 pair
Référence: 10/90
The canopy retainer set helps to keep your canopies undamaged for a long period. It absorbs movement, such as abrupt shocks in hard landings, and prevents cracks developing in the canopy.Knurled nuts are used to hold the canopy in place, and they do not intent the canopy when tightened.The components of the canopy retainer system are screwed against...
stainless steel
for turbine
Política de seguridad
Política de envío
Política de devolución
stainless steel
for turbine
Aucun avis n'a été publié pour le moment.
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: 25/9
Between fuselage and exhaust tube a heat-reflecting mat avoids melting of the fibreglass. Even in smaller fuselages where conventional silencer systems are close to the inside surface, the heat reflective mat is useful as a heat shield.Heat reflective matheat rejectingsize approx. 300 x 700 mmmat thickness approx. 3 mm
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: 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: 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.
Reference: 930/16
right / leftThis exhaust system is designed for the Mil Mi-2 with turbine power system.
Reference: 206/16
This exhaust system is designed for the UH-1D with turbine power system.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...
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: 214/16
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: 268/16
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: 429/16
Stainless steel exhaust manufactured specifically for the Bell 429
stainless steel
for turbine