Gaul Eagle French Rafale

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Reprinted from Angel Heart ^ _ ^'s blog

\In 1983 the company announced the development of advanced experimental fighter aircraft (ACX), called \
experimental \Kema push in research than 10 of the M88 turbofan engine. \February 1990 \\Later,[link widoczny dla zalogowanych], a total of five prototypes for the trial manufacture, including two Air Force-type \frame body in October 1991 to pay to do fatigue testing center in Toulouse. First a \\
Rafale A prototype

Dassault original estimates, \planes, the French Navy needs 78. Air Force's 234 in 139 is a two-seat fighter. Navy will be delivered in 1996. \Estimated price more than 60 million U.S. dollars.
Navy's Rafale M
Although the Government to formulate a multi-year procurement plan has been repeatedly delayed, but the aircraft development work has not stopped. Now the French government has finally issued the first batch of procurement plans, the first batch of production is also carried out using the test flight will soon be delivered to the user. \fighter development. The new factory of the \Particularly impressive, the French Ministry of Defense has embarked on a \
seat gust B

\lion and called the European \Although not adopted because they like the F-22 Raptor fighter fourth generation technologies, such as shape design stealth technology, thrust vectoring technology, supersonic cruise technology, but compared to the third generation of fighter aircraft now in service and use a lot of modern technology, Thus, the comprehensive combat capability has been greatly improved, and there is considerable potential for further development.
\the intake efficiency, the inlet is located under the fuselage; extensive use of carbon fiber and Kevlar fiber composite materials, aluminum-lithium alloy; diffusion bonding of titanium components / super plastic forming and other processing technology; using a threshold, automatic overload protection, fault conditions the system function and resistance to re-wire controls bump function; by side stick, fiber, voice, wide-angle holographic HUD, sight and side alignment of two multifunction color displays and other advanced equipment.
single-seat Rafale C

\wing with carbon fiber composite material. Parts of aluminum lithium alloy fittings installed. Elevons can be in the same direction and the differential deflection. The full span of two-stage titanium leading edge slats automatically linked with the elevons, the wing camber can be changed to increase the lift. Wing root fairing for the aromatic polyamide fiber composite materials. All control surfaces are fly-control system through the hydraulic steering gear.
conventional semi-monocoque body structure, 50% of carbon fiber composite material. The former is mainly conventional aluminum fuselage, rear fuselage is carbon fiber composite materials. Al-Li alloy machine body side panels. Fairing nose fairing and the nozzle for the aromatic polyamide fiber composite materials. Landing gear and engine hatch for the carbon fiber composite material. In the tail of the fuselage on both sides of front door speed brakes.
full motion before the wing is swept on the wing, hydraulically operated power transmission control system. Mainly titanium superplastic forming diffusion bonding. Landing gear down, the front wing can be automatically lifted 20 °, to provide additional lift. Carbon fiber composite cantilever vertical stabilizer and rudder using embedded honeycomb core structure. Tail tip for the aromatic polyamide fiber composite materials. Rudder control system of hydraulic power transmission control. Without auxiliary control surface. Mercier Spanish company to \Steering wheel can be hydraulically operated, before the main wheels are forward away. Design landing sink speed 4 m / s, before landing without flattening. Lin main round of the Michelin radial tire size company 810 × 275-15, tire pressure 16 × 105 Pa (16.3 kg / cm 2). Lord, carbon materials are used front wheel brakes. Power transmission control system manipulation. Emergency parachute on the rudder with a cylindrical root compartment.
Snecma M88-2 engines

its installed 2 sets of Snecma M88-2 engine, single- Taiwan static thrust of 48.7 kN with afterburning thrust of 72.9 kN,[link widoczny dla zalogowanych], optional M88-3 afterburning engine of up to 87 kN. Two independent semi-circular inlet located in the belly on both sides, no air conditioning into the cone,[link widoczny dla zalogowanych], there are manifold, the engine can ensure that the work of two non-interfering. Body aircraft capable of carrying 5,700 liters of fuel tank, fuselage centerline pylon and two wings within the wing pylons and two in 1250 liters of fuel tank can be hung, the maximum external fuel capacity up to 9500 liters, the total fuel load up to 15,200 liters. Probe in the air by the oil right in front of the cockpit windshield, B / C type is fixed, M-type is retractable. Using pressure-type fuel injection, in 4 minutes, filled with the internal fuel tank, 7 minutes, all the fuel tank full.
\Single block windshield, hatch open to the right. Hatch painted gold coating to reduce radar reflection area of the cockpit. Throttle lever with a small stroke. In the right side of the stick on the console. Abbe heat - Sai Muka's cabin air conditioning system. Two sets of hydraulic system, working pressure 280'105 Pa, the use of two Messier - Bijia Di's hydraulic pump. Frequency communication systems, there are two Auxilec 30/40 KVA alternator. A set of three redundant digital flight control system and a telex dual redundant flight control system, analog fax, integrated engine control system connected with the weapons. Eros's oxygen system.

machine uses the company Thomson-CSF has the following video / radio capability RBE2 under the radar, which can track 8 targets, can automatically Target Threat Assessment, prioritize. EAS's UHF / VHF radio and UHF radio TRT's, SB 25A and Information transceiver device, the sextant's voice radio control system and voice alarm system. SOCRAT's TLS-2020 integration of ILS / MLS, and VOR / DME systems, mechanical electrical company RL90 RLG inertial navigation systems, Thomson-CSF's NC 12E AHV 17 TACAN and radio altimeter, SFIM / electronic technology company Dassault flight recorder and the sextant's GPS system. Side-sextant's multi-function color LCD touch screen display can be integrated fuel, engines, hydraulic, electrical, oxygen and other systems of digital information, CTH3022-type wide-angle holographic HUD integrates Thomson's OTA 1320 CCD camera and VCRs. Level tactical navigation / sensor information monitor. Helmet companies Topsight sextant. Thomson-CSF company's electro-optical sensors, MIDS data link and a variety of reconnaissance, electronic warfare, forward-looking infrared and laser targeting pod and so on. In addition to the high radar warning receiver and electronic warfare equipment, the aircraft is also equipped with a laser warning system. Airborne electronic equipment and racks up to 780 kg total weight. Current \

the flight control system and structure of materials technology advances, \smaller size and weight of the aircraft. The current thinking of fighters from the traditional fighting to close from far away, medium-range missiles close combat fighting and the coexistence of the direction of transfer, so these three generations of semi-fighters are very attention to strengthening the operational effectiveness missiles, airborne radar and weapon systems require can be found as far as possible from the target, also called pre-emptive launch of weapons can be shot down each other. In this attack, in addition to track and destroy the missile's own ability, but also depends on the machine tool itself, the kinetic energy, greater energy, firing missiles can fly farther and more effective operations. At the same time the pilot must look for a \As the mother function requires the highest possible speed in the missile, so as the \In addition, because the missile's maximum transmission range also depends not only on the energy of machine tools, but also on the proximity between the enemy and double rate. Are fleeing for the enemy to attack a maximum range of the missile attack a is always less than the range of head-flying aircraft, so pilots must also be taken into account missiles quickly as possible, using energy as small as possible loss of enemy fled to avoid being counter-attack enemy missile launch. This requires \
gusts and dog fighting U.S. imperialism, the Navy's F/A-18 HUD screenshots, this large wasp of doom and gloom of the

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