Ultralight fighters.

On projects of Russian light fighter is almost no information, but apparently they exist. Is confirmed by continuing work on new small-sized motors.

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Elaboration of the Sukhoi Design Bureau in light fighter to the end of the CBS 90
Designer Konstantin Khristoforovich Marbashev ("daddy" Su-33)

Length 11.8 m

Span 8.4 m / 3.3 m

Height 3.3 m

Side view of 15.62 sq ft

View from above 29.44 m

Front view of 4 square meters

Volume of 12.25 cubic meters

Wing area 15 sq. m.

The radar "Osa" or "Spear", an antenna diameter of 0.5 m

RD-33 8300 kg / 5200 kg

Weight:

Limit 12000 kg

Max 11000 kg

Normal 10000 kg

Empty 5800 kg

Fuel 3100 kg

Load 2000 kg

Service 100 kg

Normal load two guns GS-301 and 2 P-73 (220 kg) + 2 P-77 (350 kg) + 4 UTA / LAC (300 kg) = 870 kg

Although the importance of medium-range missiles at the station with a maximum range of 50 km is questionable.

Aircraft (two versions), characterized by:

- Composition of the compositional elements: a fuselage with a cabin, swept wing, connected to the fuselage at the root of the wing and having deflected the socks in the front wing, front and tail horizontal tail, tail boom, which is located on the sides of the fuselage at the rear, dvuhkilevoe vertical tail, the air intake ;

- Location of vertical fin on the tail boom;

wherein:

- Implementation of the tail boom, is extended to the cockpit as a side stekatelya forming the root of the influx of the wing;

- On the side stekatele wing and canards;

- Location of the wing, the front and tail horizontal tail in different planes in height;

- The presence of slotted slat, located on the wings between their toes and roots;

- Implementation of the tail horizontal tail forwardswept and leading edges, trailing edges are parallel to the wings;

- Implementation of the front face of the inlet, tapered from the fuselage to the rear;

- Location of air intakes under the fuselage from the bottom of the cab before the end of the back;

- 1 st variant is characterized by continuous implementation of the wing;

- 2-th variant is characterized by the performance of the wing from the group consisting of folding together of parts.

Thrusters.

AL-55 engine thrusters on the basis of units of AL-31F, fuel consumption 28 - 32 kg / kgf * h

The main purpose of installation on training - training aircraft MiG-AT.

In the future it was planned to equip it with thrust vector control (SWT).

Later - afterburner for installation on a light twin-engined fighter, further equipping the forced option UHT.

AL-55 engines designed for the new training aircraft MiG-AT and Yak-130. Its thrust is 2000 kg (variant with afterburner thrust is 3000 kg). It is designed for supersonic speeds.

The cost - $ 500-600 thousand.

SCD-5 EDO Tumansky, bezforsazhny variant SCD-10 (MiG-35). Thrust of about 5000 kgs.
 

RD-35
 

Turbojet engine RD-35 used in the twin-engine propulsion training aircraft (TCB) Yak-130. As the base engine for the RD-35 turbofan adopted DW-2, developed for the Czechoslovak TCB A-39MS and produced in Slovakia in the enterprise Považska Stroyarne. RD-35 is produced in conjunction with Považska Stroyarne.

1-stage low-pressure compressor with two retaining steps; 
7-stage axial high pressure compressor; 
direct-flow annular combustion chamber; 
1-speed high-pressure turbine; 
2-stage low pressure turbine. 
To RD-35 introduced: 
new electronic system for automatic control system of control of technical condition; 
measures to increase life and reliability. 

Take-off thrust, kgf 2200 
Specific fuel consumption, kg / kgf hour. Take-off: 0.61
Bypass ratio 1.41 
Full extent of increase in pressure in the compressor 7.14 
Max temperature of gas turbine inlet, to 1420 
Resource hour. 6000
Dimensions, mm: 
        Length 1721
        Height 1050 
        width 994 
Weight, kg 425

RD-1700 RD-2500

Tushino Machine-Building Design Bureau "Soyuz" is finalizing the aircraft engine RD-2500
Completed design work on a new aircraft engine RD-2500, designed for installation on aircraft such as the Yak-130. About it, "Interfax-AVN said CEO - Chief Designer Tushino Machine-Building Design Bureau" Soyuz "(TMKB" Union "), Alexander Bardychev. He noted that in the construction of the aircraft engine RD-2500 uses a gas generator of the RD-1700.
"On the basis of the ongoing bench testing aircraft engine RD-1700 family of engines developed a thrust of 1.700 kg to 4.000 kg, including the RD-2500. By creating a family, we have the domestic version of this class of aircraft engines, which are currently purchased abroad ", - said A. Bardychev.
State tests of RD-2500 is scheduled to begin in late 2005.
To date, the project of creation of the RD-1700, which is the base engine for the development of the RD-2500, invested 800 million rubles. Most (90%) is the equity of industrial enterprises. In the manufacture of components for the RD-1700 RD-2500 and involved 128 Russian scientific research institutes, design bureaus and plants.
To develop aircraft engine RD-1700 will need to spend 35-38 million dollars
According to General Director of the Moscow Machine-Building Enterprise named after Chernyshev (MMP them. Chernysheva), Alexander Novikov, the completion of R & D program to create the aircraft engine RD-1700 engine-building in Tushino Bank "Union" and the serial production of the engine on MMP them. Chernysheva required to spend approximately 35-38 million
Alexander Novikov said that the RD-1700 is created for use in power-plant light training and combat aircraft. One of the aircraft to generate RD-1700, is a trainer MiG-AT.
Based on the RD-1700 family of engines designed for different purposes and thrust in the range of 1700-4000 kg. One of the engines of a draft RD-2500 to 2500 kg of thrust for the aircraft class and designation Yak-130, the source said, "AviaPort.Ru.
According to him, the distinctive feature of the RD-1700 is its almost complete interchangeability with the currently installed on the MiG-AT French Larzac engine thrust of 1420 kg.

AI-225-25 is specifically designed for the Yak-130, based on it is possible to create variants with afterburner AI-225-25F (as evidenced by all the publicity leaflets Ivchenko - Progress "). Thrust of this engine will be 4200 kg.
 

Aircraft.

The available traction of new engines largely determines the tactical - the technical characteristics of promising fighters. For a modern maneuverable aircraft with two engines, traction 3900 - 4200 kgs. Thrust each and not less than one in the first approximation:

length of 12.2 m

span 9.5 m

height of 3.6 m

wing area 26 sq.m.

weight

         Max 9800 kg

         Normal 7500 kg

         Empty 5000 kg

         Fuel 3000 kg

         load 2000 kg

Maximum speed 1800 - 2100 km / h

range without FTB 2500 - 3000 km

As an on-board radar can be installed "Mosquito -1" or "mosquito-2", weight 70 and 50 kg respectively, while shooting at up to four goals, accompanied by 24, the detection range airplane with the ESR 5 sq.m

( F-15), about 60 km.

It is known that the Mikoyan design bureau has been closely involved in the creation of Iranian light aircraft " S hafagh ", and OKB Yakovlev" engaged in the Chinese car L-15 .

Vityaz-2000

Draft aircraft Vityaz-2000 "made EDO Mukhamedov from 1994 to 2000.

Unlike JSF, "Knight" is aimed at the conquest of markets of the CIS, Central Asia and the Pacific.

EDO Mukhamedov was registered in November 1993 as the Company "Eurasia".

First, the company was engaged in trading, but later invested money earned in the study of "Composite aerodynamic configuration, in which the first patent was issued in 1994.