F/A-18E Super Hornet,

A twin shipwreck fighter, built from F-18. Because of its two role as an attack plan, it is officially recognized as F / A-18E. The highly-modified Super Hornet called the F-18E, was completed by the end of 1995 and began in 1997. The F-18E and the two F-18F seats can be easily seen by their triple injection. , Reducing radar processing and providing the strong muscle flow of their most powerful engines. F-18E is longer, has great wings and two additional hardpoints and has strong running punctuations to cope with the weight that has risen. The rate has increased by 40%. F-18E has entered the service in 1999.

Type: F / A-18E
Country: USA
Activity: fighter / attack
Year: 1999
Players: 1
Engines: 2 * 97.9 kN G.E. F414-GE-400
Wing Span: 13.62 m
Wing rating: 4
Length: 18.31 m
Height: 4.88 m
Wing area: 46.30 m2
Weight weight: 13387 kg
Max.Weight: 29937 kg
Speed: 1.8+ machines
Temperature: 15240 m (other source sources 13865 m)
Distance: 1095 km hi-hi-block bombings with 4 × 1,000 lb (454 kg), 2 × AIM-9 Sidewinder arrows, and 2 lower tanks
Travel distance: 3055 km
G-Limits: 7.6 beautiful
Power: 1 × 20 mm Canon of Vulcan of M61A1 / A2, external payment up to 8,050 kg
I-F / A-18E / F Super Hornet

Boeing F / A-18E / F Super Hornet is an anti-aircraft attack in working with the United States Navy. Super Hornet is indeed a new aircraft, which can look similar to other systems operating from the F / A-18C / D Hornet. The fighter is called colloquially as "Rhino" (with its beautiful nose). The Super Hornet was heard by McDonnell Douglas in 1992, which began in November 1995, and started in 1997 and entered the service in 1999. Current versions include F / A-18E single-seater and F / A-18F two- Stay. These replaces the old F / A-18 forms in the Navy inventory, as well as the F-14 Tomcats.

The Super Hornet kept the definition "F / A-18" for political reasons only (to get the development of new combat aircraft while Congress was not willing to support new military plans); If the plane was chosen in the correct order, its call would be "F-24A." (The definition "F-24" appears to be unpopular in politics for some reason, and it is recommended that the X-35 version be activated, adopted as F-35 Lightning II).

In the early 1990's there were several US airports. The A-12 Avenger II program, aimed at changing A-6 Intruders with A-7 and A-7 Corsair IIs, had a serious problem and canceled. The Gulf War revealed that the strike of Monday's Navy was urging the Army in some ways. Without a clean filtering system it is possible to produce results prior to 2020, to re-create the existing design into an attractive way. One such suggestion was "Super Hornet" (or, at the beginning, "Hornet II"), initially we started in the 1980s to develop the first models of F / A-18.

Compared to its predecessor, the Super Hornet has 25% large wings that allow the aircraft to return to the aircraft with a huge load of invalid memories. This was important for the use of the most expensive, well-directed weapons and growing awareness by avoiding collapse damage. Fuselage is advised to carry fuel and many avionics upgrades in the future. Over 35 percent of the engine, the General Electric F414, was developed to control these large, complex flights. The aircraft can carry 440-US-gallon (1700-liter) tanks with outdoor buses or four tanks and Aerial Refueling Store (ARS), or "buddy store," which allows the Super Hornet to renew One aircraft. Other differences include engines, a small portion of the radar cross (RCS), two additional hardpoints, and other aerodynamic changes. At the end of all of this, Super Hornet has partially allocated Fuselage's previous F / A-18 forward.

Advanced avionics presented in Super Hornet include the APG-79 AESA radar, ASQ-228 ATFLIR (Advanced Targeting FLIR), and the ALE-50 Towed Decoy System.

The electronic version of F / A-18F, EA-18G Growler, will replace the Navy's and Marine Corps' EA-6B Prowler and Raven Force EF-111. F / A-18F "F-1" was also integrated with ALQ-99 electronic-warfare system, and successfully completed the first air-conditioning of the EA-18 Airborne Air Attack Electronic Attack (AEA) November 15, 2001. Two tests of the EA-18G aircraft combined at the end of 2005, and are expected to go as assigned the designation F/A-18E (single seat) or F/A-18F (two-seat), implying that the proposal was merely a modified version of an already tried and true design. The F/A-18E/F was an outgrowth of the Hornet 2000 design study of the 1980s. The F/A-18E/F is designed to perform some of the duties originally planned for the F-14D and the A-12. One of the more important goals of the project is a 40 percent increase in the Hornet's range, which is often quoted as the Hornet's primary weakness. In order to provide more space for internal fuel, an extra fuselage plug is added, increasing the overall length of the F/A-18E/F by 2 feet 10 inches. Over that of the F/A-18C/D. The wing is proportionally enlarged by 25 percent, with an increase in wingspan of 4 feet 3 1/2 inches and an increase of 100 square feet in area. The increase in wing size is accompanied by a deepening at the roots to take extra loads. The new wing has no twist or camber and is stressed for extra operating weight. The wing of the F/A-18E/F has an outboard leading edge chord extension, leading to a definite "dogtooth" which is not present on the F/A-18C/D. By enlarging the wing area and adding a fuselage plug, 3,000 pounds of additional fuel can be carried, which is 33 percent more than the capacity of the standard Hornet. A fleet air defense F/A-18E/F carrying four AMRAAMS, two AIM-9s and external tanks would be able to loiter on station for 71 minutes at a distance of 400 nautical miles from its carrier, as opposed to only 58 minutes for the F-14D. The F/A-18E/F is provided with two extra underwing hardpoints (Nos 2 and 10) at about two-thirds of span, outboard of the existing pylons. This raises the total external stores carriage capability to 17,750 pounds. The gross weight is increased by about 11,600 pounds. The aircraft has a higher landing weight, which allows it to return to its carrier with an increased weight of unexpended ordnance (up to 9000 pounds). Increased space for chaff and flares is provided. The increase is from 60 to 120 canisters. A simplified and strengthened undercarriage is to be fitted, enabling takeoff weights as high as 66,000 pounds. The F/A-18E/F will be powered by a pair of uprated General Electric F414-GE-400 turbofans. The F414 engine is in the 20,000 to 22,000 lb.s.t. class, offering 35 percent more thrust than the F404 from which it is derived. It incorporates some of the features intended for the F412, the powerplant of the now-cancelled A-12. A completely re-designed engine air intake of trapezoidal configuration replaces the D-shaped intakes of the earlier Hornets. These intakes will provide 18 percent more air to the uprated engines and will give better performance at high speed. The area of the twin vertical fins is increased by 15 percent. The rudder area is increased by 54 percent and the range of movement is such that they can be deflected 10 degrees more, up to 40 degrees. The tailplane will be made of improved composites, and the area of the tailplanes is increased by 36 percent. The areas of the leading edge root extensions was increased by 34 percent in order to restore the degree of maneuverability at 30-35 degree angles of attack enjoyed by the current Hornet. Some stealth technology will be incorporated in the F/A-18E/F, notably on the wing leading edges to augment the beneficial effect of skinning with large areas of carbon epoxy. The radar cross section is expected to be approximately that of the F-16. The radar is to be the Hughes AN/APG-73 that is used by later-build F/A-18Cs. The single seat F/A-18E will have the 5 x 5-inch central display of the F/A-18C replaced by a new 8in x 8in flat panel active matrix LCD. The two other 5in x 5in multipurpose CRT screens are retained, as is the existing HUD, except that the control panel just below it will be replaced by a monochrome touch-sensitive screen. All displays (two CRTs, one color LCD, and one monochrome LCD) will be made by Kaiser. The rear cockpit of the F/A-18F will have identical instrumentation, except that it has no HUD and the 8in x 8in screen is located above the landscape-format touch screen. The definitive F/A-18E/F development contract was signed on December 7, 1992. It calls for three static test airframes, five F/A-18Es, and three F/A-18Fs. McDonnell Douglas opened the F/A-18E/F assembly line in St Louis on September 23, 1994. Production of the center/aft fuselage began in May 1994 at Northrop Grumman in Hawthorne, California. The Navy has assigned the name Super Hornet to the project. The prototype F/A-18E Super Hornet (BuNo 165164) was rolled out on September 18, 1995 at St. Louis. It took off on its first test flight on November 29, 1995, with McDonnell Douglas project test pilot Fred Madenwald at the controls. Aside from a minor environmental control system indication, the aircraft handled well on its first flight. Ten test aircraft were scheduled to be built, seven of which will be flight test aircraft (five Es and two Fs)

JAS 39 Gripen, Saab

Despite the smallest size, JAS 39 Gripen is an airline in fact, carrying all the equipment needed for all equipment. So one plane will be able to convert Viggen into all its versions. JAS 39 is one of the simplest of all the new generation of 90-day fighters. Its suspension is a sandal delta, enabled by the G.E. F404 engine.

Jacht Attack Spling - Fighter / Attack / Recognition) is a new venture against the purpose of taking all types of Volgens of the Royal Swedish Air Force and the existing Dear now. The Small, Agile, and Lightweight, the first delta-winged, isarad organized by the Gripen (Griffon) showcase makes its young student on December 8, 1988. JAS 39 is a wide variety of airports. Editing fighters, attacks, or recce mission types are simply made of computer software and related programs. Data is transferred to a three-down pilot MFDs and broad HUD pilot. Monitoring enemies, the MFD on the right hand of the driver is a gift-oriented data source available by the radar, FLIR, and weapons weapons. Sweden's perfect air force is on 300 aircraft to fit 16 teams.


Type: JAS 39 Gripen
Country: Sweden
Send: South Africa / Hungary
Activity: fighter / attack / recognition
Year: 1998
Players: 1
Engines: 1 * 80 kN G.E.-Volvo RM 12 (F404-GE-400)

Wing Span: 8.00 m
Wing area: 30 m2
Length: 14.00 m
Length: 4.70 m
Venue: Not Known
Wing rating: 2.13
Location Aircraft Location: N / A
Weight weight: 6622 kg
Max.Weight: 12474 kg
Internal power weight: 2,268 kg

Speed ​​Speed: Mach 1.8
The highest speed in the lowest areas: 1.15 machines
Boat Route: 3000 km (external tanks)
Radius for battle: 800 km
Grid boundaries: 9 / -3.0
Highest rate of conversion: 30 degrees / second
The maximum amount of converting is limited: 20 / second degrees
Roll rating:> 250 deg / sec
TWR (50% petrol, 2 A2A missile, 2 IR A2A missile): 0.98: 1
TWR (100% petrol, EM A2A missile 2, IR IR A2A): 0.88: 1
War: 1 * g 27 mm

Great contract: Saab Military Aircraft
Nation from: Sweden

Activity: Multi-role fighter, attack, and reconciliation
Players: 1
Year: 1988
Service year: 1997

Engine: One General Electric / Volvo Flygmotor RM12 emvaburning turbofan, 18,100 lb

Size
Wing span: 8.4 m / 27 and 7
Duration: 14.1 m / 46 ft 3 in
Max: 4.5 m / 14 ft 9 in

Weight: 14,600 lb empty / 27,560 lb max. Get up
Heat: 50,000 ft
Speed: 2,126 km / h / 1,321 mph

War: Another Mauser BK27 27mm cannon, and 14.330 lb including Rb74 / AIM-120 AAM, RB15F / Rb75 ASMs,
Bombs, rockets, weapons of DWS 39 weapons, recod / sensor pods, and fuel tanks on nine outputs

JAS 39 Gripen

JAS 39 Gripen is the cause of joint development by the Saab Military Aircraft, Ericsson Microwave Systems, Volvo Aero Corporation and Celsius Aerotech. It's the fourth generation, many fighters of war. The Gripen fighter combines new-based software-based, aircraft control systems; Modern stuff; High aerodynamic design; A well-certified engine and a fully integrated system for producing many of the most competent, most reliable aircraft. Gripen is the first Swedish aircraft that can be used to process, attack and respect (hence the Swedish JAS - Fighter (J), Attack (A) and Attention (S) dictionary in Swedish) and is currently replacing Dedicated and Viggen.

In 1978 the Swedish government ruled that the Swedish Air Force needed a new multirole plane at the end of the century. At the same time with the Swedish aerospace industry describing a new project, the Air Force conducts external exams as existing American F-16 and F-18. Following the assessment process, Parliament decided in June 1982 to proceed with the Swedish project and Defense Materiel Administration signed the JAS 39 Gripen Development Agreement, and the airline testing was completed in December 1996.

The total of 204 airports have been heard in the Swedish Air Force. The first 30 batch of the 30 airports is over. Breakdown from the second batch continues, and includes 96 aircraft and two two-seat airplanes. About 60 Gripens co-operated with the Swedish Air Force. In June 1997, the third party of 64 Gripens was approved by the Swedish Government and was ordered by Defense Materiel Administration (FMV). This will take the Swedish Air Force total at 204 airports, including 28 others. Batch production on the subject h Air Force by the Industry Group JAS (SAAB, Ericsson, Volvo Aero and FFV Aerotech) in close co-operation with the Swedish Defence Material Administration (FMV). In partnership with Sweden's Saab, British Aerospace is engaged in a number of marketing campaigns for the highly capable Gripen fourth generation combat aircraft. Engineering activity associated with improving the operability of the aircraft in the export market is now underway. In 1995 Saab and British Aerospace (BAe) signed an agreement for the joint marketing of the Gripen. Hereby, Saab gained access to the global sales organization of British Aerospace, as well as to its governmental support in international marketing. British Aerospace will adapt the export version of the Gripen to NATO standards, and also produce certain subsystems for the aircraft. The agreement, which followed on more than a decade of cooperation between the two companies, became the basis for a consolidation between Saab and British Aerospace. It also paves the way for SaabCs deepened integration with the European aerospace industry. Saab intends to be an active player along with British Aerospace, Aerospatiale (France), DASA (Germany) and CASA (Spain) in the creation of an integrated European defense and aerospace industry - Eurospace. In November 1998, South Africa announced that it will probably buy 28 Gripens. The value of the order is 12 billion SEK (1.5 billion USD) and the contract was expected to be signed in May or June of 1999. During the coming 10-15 years, Saab hopes to export at least 400 aircraft, on a total market for fighter aircraft estimated at 2,000 aircraft. The Gripen is currently being offered to Chile, the Philippines, the Czech Republic, Hungary, Austria and Brazil. Another candidate, Poland, recently announced that it will chose the F-16 C/D (block 50/52). An important factor when offering the Gripen for export, is the aircraft missile system. Currently, the Gripens used by the Swedish Air Force are armed with AIM-120 AMRAAM, AIM-9 Sidewinder, the Saab Dynamics RBS 15 for ship targets, and the Maverick ground attack missile. Saab Dynamics cooperates with the major European missile manufacturers in the development of new air-to-air missiles for the Eurofighter, the Rafale and the Gripen. The two main projects currently underway are the Meteor and the IRIS-T. The Meteor is a radar-guided, medium range (10-120 km.) air-to-air missile, which will compete with future versions of the Raytheon AIM-120 AMRAAM. The Meteor program features Matra BAe Dynamics, Saab Dynamics, Alenia Difesa, Marconi and German LFK. The IRIS-T is an IR-guided, short-range air-to-air missile, primarily funded by Germany for the Eurofighter. The project group includes Bodenseewerk Geratechnik and Saab Dynamics

MiG-29 / MiG-29OVT Fulcrum

The MiG-29 Fulcrum is air-superior fighter. It is an enthusiastic, efficient, efficient and effective aircraft, as well as the ability to use difficult aircraft. The width is a weak thing, and the latest versions were converted to carry additional gasoline. Naval version is also exploded. The Russian army seems to have chosen Su-27 major and its steps, but the development of the MiG-29M enhanced version has recently been financed. More than 2000 have been built.

Type: MiG-29 'Fulcrum-A'
Country: Soviet Union / Russia
Activity: fighter
Year: 1985
Players: 1
Engines: 2 * 81.4 kN Klimov (Isotov) RD-33
Wing Span: 11.36 m
Length: 17.32 m
Length: 4.73 m
Wing Span: 38 m2
Weight weight: 11000 kg
Max.Average: 18500 kg
Speed: Machinery 2.3
Estimation rate: 330 m / s
Heat: 18000 m
Distance: 2100 km
War: 1 * g30 mm
Unit costs: 11 million USD
Upgrade

Mig29 is one of the first Russian airports that most viewed as the same as those in the west. It included many first technologies, something that had never been seen in any western fighter. There is also a change in Russia's over the air. For example, previously the most reliable advice and guidance from the ground, so there was little of the cockpit with a very good, and as it was easy to make them have a small aerodynamic reasons as was the Mig-21, Mig-23 and Mig- 25. But Mig 29 was designed for a huge bubble bulop like those in many western cities that promote tactics.

Open doors closing the engine while it is open to the ground protects the compressor from the Foreign Object Damage (FOD). The air enters several elements into the upper part of the wing of the wing. In Mig29M (continuous development) these doors have been changed with the same grill in the Su27. It reduces corruption and creates additional space for gasoline and avionics by removing entities over the core of the wing.

Mig29 is Fulcrum-A

Mig 29 Fulcrum is equivalent to the size of the F / A-18 Hornet. It started working early in 1985 and since then it has been exported to several countries. Almost 345 of these airline guards worked with air tactical air force and 110 warriors. The Mig 29 has high flow and Pulp Doppler radar (unable to track up to 10 at once to 69km) associated with a person who receives a laser and infrared red and nomkhondo (Burst) attached to the Helmet Mounted Sight ( HMS) makes it the most outstanding time in the fighter.

Two engines eMig29 by Klimov / Sarkisov RD-33 each providing 18 ngamapounds 000. Even if one engine manifest and to provide that the Mig 29 is able to speed up one and start the engine. The engines have proved that they are able to handle as complex as the tail slides made by Anatolij Kvocur in Farnbourough in 1988.

Mig-29M / Fulcrum "E"

Mig29M has answered a lot of fighters failures. Unfortunately because of the economic position in Russia, Mig-Mapo did not get any orders for this plane. Internal storage has increased significantly; Controlled by fly fly by wire; Glass glass; New location following the Zhuk radar; Advanced engines with low-speed railways, efficiency and multiple strengths; New IRST, additional TV; Long canopy, widrow, long and lower dorsal spine; Opposition tips of the wing ngamaReceivers Warning Warning (Fore and aft) Warning Warning (RWR), eight under the wings of the wing (contrasting and 6 former ezinhumulweni); Part of aluminum lithium; And finally a larger, larger, recur roots group opposing the powerful vortices transform to bring back a space zone of a body stability and openness in increasing the angle of attack provides mobility and better performance. As you can see Mig29M is a highly developed aircraft.

I-MiG-29 OVT / Fulcrum "F"

In the MAKS in Moscow in 2001, the RSK MiG opened an assistant with guns involved. The same plane, the sixth modification MIG-29M example, is designated MIG-29OVT (Otklanyayemi Vektor Tyagi / deflected trust Vector) ", and its RD-33 engines to be installed nozzles Klimov designed to rotate up to 15 degrees in any In addition to the MIG-29-MIG-29 OVT has risen more than 2.100 kilometers, enhanced Avionics, improved weapon systems, HOTAS systems, wide range of weapons in the air and air on the ground, as well as nced steering capability. The MiG-29 OVT is the latest version of the MiG-29 jet, which has been on the market for several years. The "all-axis nozzles dramatically increase manoeuvrability, especially at low and zero speed," Vladimir Barkovsky, chief of MiG's design bureau told reporters. The demonstration of the new engine, known as the RD 33, was the culmination of several years' work. MiG started work on developing a new all-axis nozzle in the late 1990s, Barkovsky said. To date, MiG has invested several million dollars in its development. Production version of the latest MiG-29 with the proven thrust-vectoring engine that use fly-by-wire technology. The aircraft uses the same airframe of the MiG-29M1. The fighter is more agile and has an increase in range to 1,329 statute miles (2,139 km). With improved avionics, vast improvements in weapon systems, HOTAS systems, wide range of weapons of air to air and air to ground, as well as a variety of defensive and offensive avionics suite. It is no longer tied to the GCI system and would be able to conduct operations independently. It has eight weapon pylons and be able to refuel as well as carry three external fuel tanks. The aircraft is being marketed under the designation MiG-35 for potential export

F/A-18 Hornet, McDonnell-Douglas

Twin-engined shipboard fighter, developed from the smaller F-17. Because of its dual role as attack aircraft, it is officially known as the F/A-18. The F-18 is a medium-sized fighter, heavier than the F-16 but lighter than the F-14 and F-15. The RF-18 is a recce version, without the internal gun and with cameras in the nose. The USN planned to replace a lot of combat aircraft by the multifunctional F/A-18. The F-18 has also been sold abroad, to Canada, Australia, switzerland, Spain, and others. In 1999 the substantially modified F-18E 'Super Hornet' entered service. This F-18E and the two-seat F-18F can be recognized easily by their rectangular engine intakes, compared to the rounded intakes of the F-18A. It's also about 30% bigger.

Type: F-18A
Country: USA
Function: fighter / attack
Crew: 1
Year: 1980
Engines: 2 * 7250 kg GE F404-GE-400
Max.Weight: 22317 kg
Max. Speed: 1900 km/h
Ceiling: 15250 m
Max. Range: 3670 km
Armament: 1*g20mm, 7700 kg payload
Unit cost: 32 million USD
Type: F-18C
Country: USA
Function: fighter / attack
Crew: 1
Engines: 2 * 7900 kg General Electric F404-GE-402 turbofans
Length: 17.10 m
Height: 4.70 m
Wing Span: 12.30 m
Wing Area: 38 m2
Wing loading: 450 kg/m2
Empty weight: 11,200 kg
Max.Weight: 23400 kg
Thrust/weight: 0.96
Max. Speed: 1900 km/h (Mach 1.8 or 1814 km/h 11000 m)
Ceiling: 15000 m
Rate of climb: 254 m/s
Max. Range: 3330 km
Armament: 1*g20mm M61 Vulcan internal gatling gun with 578 rounds, 6220 kg payload
Unit cost: 32 million USD
Type: F-18E
Function: fighter / attack 
Year: 1999
Crew: 1
Engines: 2 * 97.9 kN G.E. F414-GE-400
Wing Span: 13.62 m
Length: 18.31 m
Height: 4.88 m
Empty Weight: 13387 kg
Max.Weight: 29937 kg
Speed: Mach 1.8+
Ceiling: 15240 m
Range: 
Armament:

F/A-18A/B, C/D Hornet

Description:
 All-weather fighter and attack aircraft. The single-seat F/A-18 Hornet is the nation's first strike-fighter. It was designed for traditional strike applications such as interdiction and close air support without compromising its fighter capabilities. With its excellent fighter and self-defense capabilities, the F/A-18 at the same time increases strike mission survivability and supplements the F-14 Tomcat in fleet air defense. F/A-18 Hornets are currently operating in 37 tactical squadrons from air stations world-wide, and from 10 aircraft carriers. It is proudly flown by the U.S. Navy's Blue Angels Flight Demonstration Squadron.
Features: The F/A-18 Hornet, an all-weather aircraft, is used as an attack aircraft as well as a fighter. In its fighter mode, the F/A-18 is used primarily as a fighter escort and for fleet air defense; in its attack mode, it is used for force projection, interdiction and close and deep air support.
Background: The F/A-18 demonstrated its capabilities and versatility during Operation Desert Storm, shooting down enemy fighters and subsequently bombing enemy targets with the same aircraft on the same mission, and breaking all records for Tactical aircraft in availability, reliability, and maintainability. The aircraft's survivability was proven by Hornets taking direct hits from surface-to-air missiles, recovering successfully, being repaired quickly, and flying again the next day. The F/A-18 is a twin engine, mid-wing, multi-mission tactical aircraft. The F/A-18A and C are single seat aircraft. The F/A-18B and D are dual-seaters. The B model is used primarily for training, while the D model is the current Navy aircraft for attack, tactical air control, forward air control and reconnaissance squadrons. The newest models, the E and F were rolled out at McDonnell Douglas on Sept. 17, 1995, and are currently undergoing further testing at the Patuxent Naval Air Station in Maryland. The E is a single seat while the F is a two-seater.
All F/A-18s can be configured quickly to perform either fighter or attack roles or both, through selected use of external equipment to accomplish specific missions. This "force multiplier" capability gives the operational commander more flexibility in employing tactical aircraft in a rapidly changing battle scenario. The fighter missions are primarily fighter escort and fleet air defense; while the attack missions are force projection, interdiction, and close and deep air support.
The F/A-18C and D models are the result of a block upgrade in 1987 incorporating provisions for employing updated missiles and jamming devices against enemy ordnance. C and D models delivered since 1989 also include an improved night attack capability.

General Characteristics, C and D models

Primary Function: Multi-role attack and fighter aircraft
Contractor: Prime: McDonnell Douglas; Major Subcontractor: Northrop
Unit Cost: $ 24 million
Propulsion: Two F404-GE-402 enhanced performance turbofan engines
Thrust: 17,700 pounds (8,027 kg) static thrust per engine
Length: 56 feet (16.8 meters) 
Height: 15 feet 4 inches (4.6 meters)
Maximum Take Off Gross Weight: 51,900 pounds (23,537 kg)
Wingspan: 40 feet 5 inches (13.5 meters)

North American B-70 Valkyrie

The B-70 was a high-flying Mach 3 bomber, intended to replace the B-52. It was a canarded delta wing aircraft, designed to 'ride' on the shock wave contained between the lower fuselage and its movable, downturned wingtips. Because of kinetic heating at high speed, the B-70 was built from titanium and steel honeycomb parts. The advent of surface-to-aircraft missiles made the high-flying bomber obsolete. Two were built, as two-seat research aircraft.

Type: XB-70
Country: USA
Year: 1964
Crew: 4 (pilot, copilot, bombardier, and defensive systems operator)
Engines: 6 * 13075 kg G.E. YJ93-GE-3
Wing Span: 32.00 m
Length: 59.75 m
Height: 9.22 m
Wing Area: 585.43 m2
Empty Weight: 92990 kg
Max.Weight: 249470 kg
Speed: 3200 km/h
Ceiling: 22860 m
Range: 9650 km
Unit (prototype) cost: $700 millions
Armament: No defensive weapons except ECM. Internal bay for up to 14 nuclear or thermonuclear bombs, or an assortment of conventional bombs. Externally carried stand-off missiles were also considered.
With research and development studies beginning in 1955, the XB-70 was a large, long-range strategic bomber was planned to be the replacement for the B-52. As in the B-58 program, the Air Force wanted new technology advances. To this end, the Air Force gave the prime contractor total weapon system responsibility. Competition between Boeing and North American for the contract occurred during the design phase. In 1958, the North American design was chosen and a development contract awarded. The Air Force requirement was for a Mach 3, high-altitude, long-range bomber capable of carrying nuclear and conventional weapons. Although there was a technology breakthrough in 1957 that made Mach 3 possible, the XB-70 never went into production. The continuing emergence of new SAMs was the key factor in the demise of the XB-70, just as it affected the B-47 and B-58.

The XB-70 had a length of 196 feet, a height at the tail of 31 feet, and an estimated maximum gross weight of 521,000 pounds. It had a crew of four: pilot, copilot, bombardier, and defensive systems operator. The delta wing had a span of 105 feet with six turbojet engines side by side in a large pod underneath the fuselage. The wing was swept at about 65½ °, and the wing tips were folded down hydraulically 25o to 65o to improve stability at the aircraft's supersonic speeds of up to Mach 3. At this speed the Valkyrie was designed to ride its own shock wave. A large canard foreplane near the front of the fuselage with a span of 28 feet, 10 inches was used for stability. In addition to its sharply swept delta wings, the XB-70s had two large vertical tails. The aircraft was fabricated using titanium and brazed stainless steel "honeycomb" materials to withstand the heating during the sustained high Mach number portions of the flights. The propulsion system consisted of six General Electric turbojet engines (J93-GE 3) with two large rectangular inlet ducts providing two-dimensional airflow. 

The entire mission (including return) was to be flown at Mach 3, but even then the aircraft was vulnerable to SAMs of the 1960's vintage. A high altitude, Mach 3 penetrator cannot maneuver well; its straight and level trajectory would have been an easy course to plot and intercept. Further, the technology that made Mach 3 possible yielded an airframe with a large RCS that added to the effectiveness of SAMs against the XB-70. The airframe was not adaptable to low level penetration to avoid SAMs because the delta wings were very thin and did not lend themselves to the structural modifications necessary for sustained, low level flight. 

The XB-70 design had payload flexibility but not mission flexibility. In 1959, the XB-70 concept was changed to a recon/strike RS-70, making it a reconnaissance aircraft with a bomber strike capability. However, its reconnaissance capability would not have been as good as the super high altitude aircraft designed to fill the reconnaissance role. The XB-70 was an aircraft which fulfilled the criteria it was designed to meet, but whose mission had been eliminated by defensive threat technology. The high drag of the Mach 3 airframe required a fuel load comparable to the B-52 but limited the range to about 5,000 nm. It was capable of carrying both conventional and nuclear weapons internally, but due to its design and Mach 3 mission profile, it could not carry external ordnance. 

In 1961, President Kennedy announced that the XB-70 program was to be reduced to research only, citing high cost (over $700 million per prototype) and vulnerability. The Kennedy administration felt ICBMs were more cost effective because they were less vulnerable and were cheaper operationally. Although two XB-70 prototypes were built, with the first flight in 1964, the program terminated in 1969. The XB-70 had speed, range, and adequate payload, but it was expensive, not suited to low level penetration, and thus did not compete with ICBMs for strategic funds.

Rafale, Dassault-Breguet

Fighter for the next generation. France decided to upgrade its fighter, reject European EFA as much as possible in the use of the work and is very expensive to export. Click with the sandal delta, but it has EFA rows below. Broad use is made of building materials. Rafale A was a reflection, Rafale B is the version-seat, Rafale C one, and the Rafale M version fighter version. There were four graduates who flew in early 1997. The 272 production of Orders of France's animal species are expected.

France chose to produce Rafale, who will be operating in 1999, instead of Eurofighter. Easy is simple and smaller than Eurofighter. It will be produced in three versions: Rafale M, Rafale C, and Rafale D. The M is a carrier, with a wheelchair that holds the spring in order to get rid of the air when it starts. C is one unit and D is a small version of force in the air.

Type: soften C
Country: France
Send: N / A
Activity: Multi-role fighter
Year: (1997)
Players: 1
Engines: 2 * 77 kN SNECMA M88-2

Wing Span: 10.90 m
Length: 15.30 m
Height: 5.34 m
Wing area: 46.0 m2
Wing rating: 2.6
Venue: Not Known
Location Aircraft Location: N / A

Weight weight: 9060 kg
Max.Average: 19500 kg
Internal Fuel: 4000 kg

Speed: Mach 2.0
Temperature: 18290 m
Boat type: 3125 km
Radius fighting: 925 km
Grid boundaries: 9 / -3.2
High speed change rate: 30 degrees / second
Highest rate of conversion: Not known
Rollrate: 270 degrees / a minute
TWR (50% gasoline, 2 A2A missile, 2 IR A2A missile): 1.3: 1
TWR (100% fuel, EM-A2A missile 2, IR IR-A2A missile): 1.10: 1

Battery: Internal internal 30 mm Giat DEFA 791B cannon. External size up to 6000 kg (13.230bb) 6 under underwing, 2 wingtip, 2 centerline, and 4 floating channels. Options include ASMP equipment for missoff standoff, up to 8 Matra Mica AAMs, AM 39 Exocets, LGBs, ASM LGLMs, or Apache suppliers with anti-anti-anti-anti-antibiotics.

Unit costs: million million USD
MEMBERS OF THE PEOPLE IN THE ACT OF THE LAW (November 2002)

Rafale from France has a fire, but will she still boast?

Dassault Rafale is a small aircraft (does not need to force the wings to match the carrier) with a heavy load. Rafale has a weight of about 20 pounds [22,000 kg] and originally made a weight of about 49,600 pounds [49,600 kg]. This amount has risen to 54 pounds [54,000 kg], and Dassault is preparing to break up to 60,000 pounds.

Apart from fats or weapons, Rafale weighs up to 3 pounds [3,000 kg] above F-16C, but can weigh up to 10 pounds [10 kg]. This allows Rafale to wear 21,000 pounds [21,000 kg] in stores in addition to over 9,000 pounds inside internal pipes. In tank machines with fuel supplied with US 600 600 liters of electricity - made and tested by Dassault while its winning Korean competition - Rafale could run a 1-nm radius strike, carrying a lot of air-weapons Weapons and air arrows. Despite these skills, Rafale failed to conquer one export order, despite the fierce opposition campaigns in the United Arab Emirates and Korea. Singapore approaches the decision on high-level sailors. Lockheed Martin F-35 Lightning II Joint Strike Fighter (JSF) is obviously facing the world market available, at least so far, so Singapore, seeking aircraft before the JSF is ready, is a unique opportunity for European opponents, as the Eurofighter Typhoon and the competition French, Rafale.

Meanwhile, by the end of August, Rafale's oldest partner, Mirage 2000, has been running for the first 24 aircraft in Brazil, with 36 other aircraft that may be sold at the next auction. Since the early 1990's, Mirage has been incorporated into the vast range of technologies built at the beginning of Rafale - even some of the main features - and the Mirage and Sweden of Gripen (see "Heavenly Rock," JED, April 2002) The most successful arguments From a United States person who had been involved in the business fighter.

Rafale, like most of her days, has taken longer to improve than expected. Rafale A technology director made his first flight in July 1986. After a discrepancy between France and four countries of Eurofighter, the French government decided to continue to fully comply with Rafale's development in 1987. Protocols go It is organized by other projects - the Navy airline Cyrus de Gaulle and the Army's Tiger helicopter, for example - a complete and flexible budget, leading to a significant delay in the production of money. However, Navy's needs are urgent, and Rafale M based on the company's carrier has become a unique alternative to Rafale. Rafale's first team, Flotille 12F, was formed in May 2001 and is currently climbing Charles de Gaulle. Seven airports are shipped to the Indian Ocean at the beginning of this summer, and the group is expected to be fully reported, as well as ten airports. According to French officials, some illegal training talks have already occurred between Rafael and the US Navy F / A-18. On June 9, 2002, Rafale Ms of the French Navy working on Charles de Gaulle participated in a joint venture with the American fighters. Although the assignment was respected at the Indian border of Pakistan and no firearms were issued, it became clear that the official debut of the airport (see "Make Two Partnership," JED, August 2002). The 20 airline announcement announced at the end of 2001 brings 61 strict aircraft restrictions (36 French Air Force and 25 Navy). The first 13-batch breakdown-including Rafale Ms of the 10-year-old Navy and Rafale Bs two Air Force tests for Air Force - has already been completed. One plane must be submitted in January 2006, and another 20 must be followed in February 2007. The first operating aircraft will reach the French Air Force in March 2004, and the first phase of operation should be in 2006. Rafale is 294: 60 Rafale M and BM's Navy, 139 lower-ground aircraft and 95 air-conditioned Air Force seats. The current system calls for deliverance to continue until 2019. High voltage Thales RBE2 radar is an electronic-scanned-type type (ESA), such as B-1 of Northrop Grumman APQ-164, with one source of power, the sender, Recipient, and the suspension phase chemicals to direct the volume. The radar has one handle - unlike the applicable ESA used for F-22 and JSF - but it can be displayed immediately in any way to use a variety of ways. Dassault describes as the difference between the "track while scanning" and "follow here while you're scanning there." For example, RBE2 can follow non-winding texts while looking for solutions to the ground or providing a global airline profile. ESA sacrifices are not compatible with sympathy with the active category or radars in the form used in Gripen and Typhoon. However, according to Dassault, passive array has been selected by the original versions, since the customer needs the ability to distinguish different approaches, and the operating list is far off matured. Also, the French Air Force operates on AWACS's oldest aircraft, while the Navy has E-2C Hawkeyes, which is caused by the worst vision distance. The radar is supported by visual and electronic systems of detection. It has been discovered immediately after the radar is the optronic (FSO) system, produced by Thales. The FSO has two optical headings. On the right are long and long-distance infrared searches (IRST), operating on the long-wave IR band, receiving IR resources beyond the broad viewing platform. Left is the sensor-identification identifier, which combines the sensation sensor (sunshine in the exhibition and the community between the IR in the aircraft) as well as the laser rangefinder. It can track one feature in the previous field and display an enhanced image on the cockpit, and it is usually targeted in the most threatening container. If the rules of engagement require identifying the material, the Rafale driver can announce the goal as a malicious source without a standard visual view. Information from Spectra EW suite, radar, and OSF are combined together on modular computers and submitted to the airline and the backpack with a modern cockpit with square in square 160 of active display space - half to an inch -180 square In the F-22 larger and more than the storm. The harfare of the Rafale cockpit covers many unique or unique features. The main interior screen, which normally holds a great tactical-state signal, is compiled with endless collimated. The body optics for "high-performance" (HLD) is designed to be higher than the HLD directly under the headset (HUD). (In most other fighters, there is a small control panel

B-2A Spirit stealth bomber

On November 22, 1988, B-2A is a stealth high-speed gun from the 1978 program. The first prototype of 6 made its flight flight on July 17, 1989 with an extermination test in 1997. -2 is equipped with a 'pedal wing', with the edges along with the surrounding edges to help distort the radar. Exhausts in the upper and upper part of the unit are helping to reduce infrared signals. The USAF plans to get a plurality of 20 B-2A airports.

B-2 will probably be created only with smaller numbers (currently 21 are ordered), because the cost of installing all the B-52 elements is considered to be too high. B-2 is a stealth bomb, a design of high-speed, wooden plane, but angular wing and double-W sequences. These four engines are deeply buried in the reduction phase. B-2 is difficult and cost effective, and 124 hours of repair by hour driving.

ATB development (Advanced Technology Bomber) began in 1978; The program was publicized in 1981, when Norroprop design was selected on Lockheed / Rockwell's advice. Although the design of the designs was not visible, it was widely thought that the plane would be "an airplane", based on the experiences of Norththrop and XB-35 and YB-49, and this was confirmed when the first exhibition was released on November 22, 1988. Make its first flight on 17 July 1989, and the first production B-2 was awarded to the USAF in 1993. Production plans have been severely reduced from 135 to 20 flights, which will be expected to be released in 1997. This aircraft was called "Spirit" in February 1994; Northrop was Norththrop Grumman in May 1994.

Vital figures (B-2A): length of 21.03 m, range of 52.42 m, empty weight 72575 kg, empty weight 168434 kg, maximum speed 1103 km / h, 13898 km, uploaded 22370 Kg; Power plant: four 84.51 kN General Electric F118-100 in Turbofans.

On February 23, 2008 a B-2 bomb crash in the Guam area after leaving, but both drivers were safely driven.

Contract contract: Northrop Grumman Corporation
Nation from: USA
Activity: Strategic stealth ball
Coaches: 2/3
Year: 1989
Year of operation: Complete discontinuation in 2000
Engine: General General Electric F118-GE-110 non-watch turbofans, 19,000 lb progresses
Wing span: 52.43 m
Wing area: 465.5 m2
Length: 21.03 m
Size: 5.18 m
Weight: 168434 kg
Temperature: 16765 m
Speed: 1103 km / h
Distance: 18,520 km per one airel
War: Up to 80,000 lb including 16 B61 / B83 weapon bombs, 80 Mk82 1,000 lb bomb or Mk84 2,000 lb bomb, 36 M117 750 lb fire bombs, 36 bombings, or Mkk -1 lb.
Unit costs: 800-1300 million USD
Mission

The spirit of B-2 is a multinational force capable of bringing both natural and nuclear weapons. A major technological emergence, the bomb represents the most important step in the current U.S. system. B-2 brings great power to catch fire, in a short time, anywhere in the world through the impossible protection.
Features

With B-52 and B-1B, B-2 provides flexible and efficient variables from human bombs. Its seemingly low, or "bad" symptoms, provide unique ability to enter the enemy's defense and threaten its most valuable, most secure purposes. Its ability to enter into air protection and threaten effective retaliation has given strong, effective and effective forces to fight during the 21st century.
The compact appearance of a small visual technology with excellent energy efficiency and high-paying payout offers the most important B-2 benefits over existing guns. Its lack of foresight gives great freedom of action to the highest places, thus increasing its range and better aircraft aircraft. Its total range can be 6,000 square miles [9,000 km] nautical (9,600 km). The lowest view of B-2 depends on the integration of infrared, acoustic, electromagnetic, visual and radar. These designs make it difficult for these complex systems to find, trace and engage in B-2. Many features of the lowest process of keeping them are always separated; However, B-2 construction materials, special dressing and the design of all swimsuit wings play a part in "behavior."

B-2 has a team of two operators, the airline on the left side and the military commander on the right, compared to the B-1B staff with five B-52 employees. Thend Joint Air-to-Surface Standoff Missile. B-2s, in a conventional role, staging from Whiteman AFB, MO; Diego Garcia; and Guam can cover the entire world with just one refueling. Six B-2s could execute an operation similar to the 1986 Libya raid but launch from the continental U.S. rather than Europe with a much smaller, more lethal, and more survivable force. Background The B-2 development program was initiated in 1981, and the Air Force was granted approval in 1987 to begin procurement of 132 operational B-2 aircraft, principally for strategic bombing missions. With the demise of the Soviet Union, the emphasis of B-2 development was changed to conventional operations and the number was reduced to 20 operational aircraft, plus 1 test aircraft that was not planned to be upgraded to an operational configuration. Production of these aircraft has been concurrent with development and testing. The first B-2 was publicly displayed on Nov. 22, 1988, when it was rolled out of its hangar at Air Force Plant 42, Palmdale, Calif. Its first flight was July 17, 1989. The B-2 Combined Test Force, Air Force Flight Test Center, Edwards AFB, Calif., is responsible for flight testing the Engineering, Manufacturing, and Development aircraft as they are produced. Five of the six developmental aircraft delivered to Edwards are still involved in continuing flight testing. The first test aircraft is currently kept in flyable storage. Whiteman AFB, Mo., is the B-2's only operational base. The first aircraft, Spirit of Missouri, was delivered Dec. 17, 1993. Primary maintenance responsibility for the B-2 is divided between Oklahoma City Air Logistics Center at Tinker AFB, Okla. for avionics software (contractor); Ogden Air Logistics Center, Hill AFB, Utah for landing gear and trainers (contractor); and the Northrop-Grumman facility at Air Force Plant 42 at Palmdale for periodic depot maintenance. The prime contractor, responsible for overall system design and integration, is Northrop Grumman's B-2 Division. Boeing Military Airplanes Co., Vought Aircraft Co., Hughes Radar Systems Group and General Electric Aircraft Engine Group are key members of the aircraft contractor team. Another major contractor, responsible for aircrew training devices (weapon system trainer and mission trainer) is Hughes Training Inc. (HTI) - Link Division, formerly known as C.A.E. - Link Flight Simulation Corp. Northrop-Grumman and its major subcontractor HTI, excluding Link Division, is responsible for developing and integrating all aircrew and maintenance training programs.

Sukhoi Su-35 Super Flanker

Improved 'glass cockpit' version of the Su-27, with canard foreplanes, more powerful radar, more powerful engines, and possibly thrust-vectoring nozzles, and an electronics upgrade. The Su-35 has a completely new FCS from that on the Su-27. As well as canards, it has a new, square-topped tailfin (with internal fuel tanks). It also has a new N-011 radar with a range of up to 400 km (or 200 km against ground targets) which can simultaneously track more than 15 targets, engaging six. The new EO complex gives compatibility with advanced "smart" weapons. An advanced datalink allows coordinated group operation and the tailcone houses the antenna for a rear-facing radar which will allow "over-the-shoulder" missile shots. The Su-35 will be compatible with the new 400-km Novator KS-172 AAM-L missile. Flight testing in now reportedly complete and production has been funded. The Su-35 looks a lot like the Su-33. Consideration is being given to retrofit Su-35s with thrust vector control as seen in the Su-37.

Type: Su-35
Country: Soviet Union / Russia
Year: 1994?
Crew: 1
Function: fighter
Engines: 2 * 137.3kN AL-31MF
Wing Span: 15.16 m
Length: 21.96 m
Height: 6.84 m
Wing Area: 62 m2
Empty Weight: 18400 kg
Max.Weight: 34000 kg
Speed: 2440 km/h
Ceiling: 18000 m
Range: 3500 km

YF-23 Black Widow II, Northrop/McDonnel Douglas

The YF-23A body is a combination of powerful shaping and aerodynamic performance, hoping to provide radar cross section without compromising performance. YF-23A was too long and easier than Lockheed YF-22A. The main waste disposal structure, measured from the stablizer to the front of the pulpter, is approximately 7 feet [7 m] higher than the YF-22A. From the side, the YF-23A profile reminds you of that of Lockheed SR-71. Normal sighting in other angles is that the person is tall, high in the middle of different different nacelles in the engine. Differential lengthwise in a fractional area is extremely smooth, reducing transonic and supersonic pulling. The upper phase has a cross-sectional cross-trapezoid cross-section, one above the image in the mirror, in the aft region integrated into a circular section and disappears within the back fuselage. The upper part of the engine box is controlled by two nacelles such as the well-wing nacelles, each nacelle being part of the changed trapezoidal cross. The front holder holds a cockpit, gear gear gear, electronics and missile bay. YF-23 nacelles were higher than they would have in producing F-23, because they were designed to assist the ATF's first-edited transformers but were subsequently deleted.

Spiral plants such as trapezoid are available under each wing, which are the leading edge of the simple-geometry lip in the system-shock system. The inclusion of wings beneath the wings is beneficial for removing fuselage sides so that the maximum border boundary is required. Instead, a small layer of boundaries inserted into the front of the memorial was removed by a burning panel and opened over the wing. The entrance door on the side of the inlet is at each level of the above particles in front of the engine to provide additional air to the low-speed or low-speed drills. Incoming tires lead to the second half of the engines, up and down, to protect the face of compressors from the best radar machines.

The leading edge of the YF-23A wing has been back to 40 levels, and the tracking limit goes on for the same hour. When viewed from above, the wing has this program for the defeated group. At YF-23A, all lines on the wall are accompanied by one or the other at the end of the dispute, which has been one of the guiding principles in the strongest design. The wing is made deep, and there is enough room to cook inside the wing box.

The wing has slats leading to more than two thirds passages. The tracking border has an internal flaps set and a set of drooping ailerons out. Unlike Lockheed YF-22A, no bookmark suitable for YF-23A.

V-twin twin V-muscles are farther away from the back fuselage. There are 50 degrees that are out of the effort to avoid small leaves or right angles in forecasts or forecasts. These all tailor sections are combined with one pivot. Their leading and successive ends are like big wings but on another plane. Two aircraft sounds as a motorcycle that comes from all angles except those above or above the airplane.

In YF-23A, Northrop is selected not to use a thrust-vectoring for aerodynamic control. This is done to save weight and help to achieve all the stealth aspect, especially from the background. All controls are on aerodynamic areas. V sounds apply to pitch, roll, and yaw. Continuous movement patterns provide roll roll and lift up augmentation, but they operate as speedbrakes and rudders. To correct straight lines, the control system commands external ailerons to disagree and the internal points to inflict on the ground, thus generating a refinement but can create other times. Yaw management can be provided by doing this on the other hand.

There are burdens for removing waste from the existing fuselage body after the driver's license. As part of YF-22A, YF-23A has a fly-by-wire system that controls living environment settings that respond to the driver's responses.

Therapeutic treatment is stored in fuselage after a person, where a combined tail bag is combined between the two V-tails and includes an exhaustive engine in a low RCS system. Unlike YF-22A, YF-23A does not use prector vectoring. Exit bridges forward to the upper fuselage, between the tails,

EuroFighter Typhoon / EF2000

The first flight is an example Eurofighter Typhoon took place on March 27, 1994, when Messerchmitt Bülkow-Blohm (MBB) chief test pilot Peter Weger took the example of a flight test in Bavaria. The basic configuration is reminiscent of the British Aerospace (Bae) EAP agile combat aircraft show, which returned in August, 1986. In fact, the EAP was used to check the number of Eurofighter before the final flight configuration final was decided. (Relationship is like F-17 and F / A-18, where the base system is similar but many changes have been made.)

The EuroFighter, known as the EF2000, was built by BAE (UK), MBB and Dornier (Germany), Aeritalia (Italy), and CASA (Spain) consortium. Initially, there are rooting and winding roles, but the changing world situation has achieved a strong emphasis on the air and the air.

The STOL (Short Take-Off and Landing) plane has an inexpensive design of aerodynamics; While this requires airlines flying, it offers high Eurofighter power. Each of the best turbofans Eurojet EJ200 offers 20,250 pounds [20,250 kg] of afterburning thrust; With a maximum weight of 37,480 pounds [37,480 kg], this means that Eurofighter has the power to save. Although it's not a stealth flights, carefully crafting and use of composites and low detectability (the surface of the airframe technology only 15% of the metal) Eurofighter is light and has a profile radar much smaller than the 1980-era fighters.

The system control fly-by-wire ensures the driver can stall or overstress the airplane, and there's even a button that will automatically restore the aircraft wing-level, nose-up attitude if the pilot becomes disoriented after the G level of mobility. All important changers are suggested in the pit or cord, giving the HOTF real-time Eurofighter (hands-to-face and elevator). The three MFDs are raised with panels combined with the HUD and the display of an ASRAAM shooting helmet.

Researchers often admit that the only fighter facing Eurofighter is American F-22, which is double and has no EF2000 power.

The Eurofighter is the product of a consortium of British Aerospace, Deutsche Aerospace (Germany), the sum of (Italy), and Casa (Spain), and the United Kingdom and Germany providing technological leadership. Under development since 1988, fully Eurofighter is a 46,000 lb, -isihlalo a single, twin-engine from a short period of time and remains in the (installation) multirole fighter, which is optimized for air superiority in both the visual-range (BVR) missile with the ability to close -ukulwa physical activity, but also skilful That works in the air. Computer use (focusing on BVR air-to-air combat) by European contractors and government agencies suggests that Eurosighter is superior to U.S., Russian, and European fighters are being investigated, outside of F-22. Although it is not possible to assess the availability of the findings, they show that Eurofighter developers are targeted with the highest capabilities.

Eurofighter Typhoon is a twin-engine multi-role indirect-delta strike against aviation, designed and built by the European airline operators, the Eurofighter GmbH, built in 1983.

The production of the Eurofighter Typhoon series is now continuing to operate legally with the Italian Air Force. 'Starting Performance' is expected to be announced by Germany, Spain and the United Kingdom in 2006. Austria has bought 18 storms, while Sadi Arabia has been signed on 18 August 2006 to 72 by BAE Systems.

Technical writing

Eurofighter is a product of four national organizations made up of UK, Germany, Italy and Spain. The Eurofighter program began in 1983 with a desire to produce an aircraft that could be used in global protest until the 21st century. The developmental development started with the EAP (The Air Testing System) in 1988. In March 1994, the first move of EF2000 occurred. EF2000 is now used for RAF delivery in 2003.
Eurofighter is a bulletin car collected by a delta aircraft that is challenged to lift air but can be used for land attacks. The extensive use of high-tech devices has been made including carbon components, plastic reinforced glass, titanium, and aluminum lithium, 80% of the airframe. Like Gripen and Rafale EF2000 utilizes the extensive delta program documents and components to get the best combination of performance, lifting, and speeding.

The cockpit condition is one of the most advanced in the world using flying fly-by wire anD multi-function displays. The Twin EJ2000 stimulates turbofans that provide a powerful but effective operating system. Improved weapon makes EF2000 a deadly enemy to any enemy.
Armament

The Eurofighter carries NATO's best weapons. It has a high load Capacity with flexible missile configurations. It has thirteen carriage points, three of which are capable of holding external fuel tanks. The maximum fuel or weapons payload is 6,500 kg (14,330 lb.). A mixture of at least ten ASRAAMs (advanced short range air-to-air missiles) and AMRAAM (advanced medium range air-to-air missiles) can be carried with four of the AMRAAMs housed in low drag, low observability fuselage stations. A wide variety of air-to-surface weapons can be carried on seven stations, including avionics stores such as laser designators.