[السادات]

سلام عليكم إليكم مواصفات التايفون
بالشكل الجديد
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الأنظمة
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Secondary Power System

The Secondary Power System (SPS) enables the hydraulic and electrical systems, and engine starting. It consists of an Auxilliary Power Unit (APU) and two engine-driven gear boxes.
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Utilities Control System

Dramatically reducing pilot workload, the Utilities Control System (UCS) provides continuous control monitoring and fault detection for the aircraft''s general systems, and also acts as an interface in the avionics architecture.
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Hydraulics System

Two separate, independent hydraulics systems are incorporated in the aircraft, supplying various items, such as the canopy, FCS, brakes and undercarriage. One 4000psi engine-driven gearbox powers each system.
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Fuel System

Fuel is contained in the centre fuselage and wings as well as the external, underwing drop tanks. A retractable refuelling probe is mounted on the starboard front fuselage.
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Electrical System

The system is designed to minimise the risk of total power loss by using a high level of redundancy and system partitioning. Power provided is 115/220v, 400Hz,
3 phase AC, 28v DC.
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Environmental Control System

The Environmental Control Systems (ECS) provide conditioned and partially conditioned air to the cockpit canopy seal, anti and demisting systems, anti-g suit, as well as to radar, FLIR and avionics sub-systems.
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Defensive Aids Sub System

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وأخيرا ما تفاجأت به و جود تواجد إضافية
كما هو الحال في الاف-16

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تقريبا أصبحت هنا كأنها تحمل 5 توانك كل تانكي فيه 2000رطل
أي 1000 لتر بالتالي أصبحت 5000 لتر بدون الخزان الداخلي
طبعا ممكن يكون تانكيين 1500 لتر كل واحد
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