Mikoyan MiG 1.44 MFI

Wings

The MiG 1.44 had Delta wings. Delta Wings are wings shaped in the form of triangle and was named after its similarity to the Greek uppercase letter delta(Δ). The MiG 1.44 had a wing leading edge of 40-45° Degrees.

Wingspan

49.2 Feet

Length

62.3 Feet

Height

14.8 Feet

Wing Leading Edge

The Angle of which the front of the wing is at.

Engines

2 Thrust-Vectoring Lyulka-Saturn AL-41F afterburning turbofan engine giving out 39,680lbs thrust each. The engines would allow the MFI to "super cruise" meaning it could go without afterburner thus increasing range. It can go MACH 1.5 in super cruise.

Thrust Vectoring

The MiG 1.44 has thrust vectoring nozzles which vector thrust from the engines. This gives the MiG 1.44 the ability to have high angles of attack of atleast 60° Degrees.

It is Empty and just a Fighter Jet

It is just an empty fighter craft, nobody is in it and bares no consciousness.

Primary Armament

30mm Izhmash GSh-301 cannon which would of fired 30mm by 164mm at a rate of 1,500 to 1,800 Rounds Per Minutes.

Empty Weight

39,683 Pounds

Maximum Take-Off Weight

77,162 Pounds

Variable Engine Intake Ramp

Located under the fuselage, the Variable Engine Intake ramp would allow countinus airflow in the the Engines during sudden maneuvers.

Radar Cross Section

It would have a Radar Cross Section or RCS for short. It would have a RCS of 0.3 meters²

Control System

It would use a Fly-By-Wire system for more enhanced maneuverability and a much much smoother flight and quicker reaction time so the aircraft can preform sudden manuvers.

Canards

The MiG 1.44 would have a close-coupled layout giving the aircraft maneuverability equal or better than the F-22.

Manufacturer

Mikoyan-Gurevich

Service Year

1999

Secondary Armaments

The secondary armaments that would be held on plyons located under the wings and a weapons bay in the fuselage. It would have had 4 Wing Plyons and an internal weapons bay capable of housing 12 missiles. Likely the AA-12 "Adder" a medium range, radar guided missile, and the AA-11 "Archer" a short range, infra-red guided missile. It could likely also have held the K-37 a long-range, radar guided missile and the K-74 short range, infra-red guided missiles.

Maximum Speed

MACH 2.35 or 1716 Miles Per Hour

MFI

MFI stands for "Mnogo-Funktsionalniy Istrebitel" or "Multi-Role Fighter"

Names of the MiG 1.44

Mikoyan MiG 1.44 MFI, Mikoyan MiG 1.44, MiG 1.44, MFI, and Flatpack.

Country of Origins

Soviet Union(Before it collapsed in December 26, 1991) and Russia

Radar

It would use the Pulse-Doppler Radar, the N014 Radar which has a range of 260 miles and a target detection of 160 miles to 3.3 feet, it was able to track up 40 targets and shoot against 20.

Basic Principles of Fluid and Lift

Lift is generated by an Airfoil(The Wing of an given aircraft) by generating low pressure under the curvature of the wing, and high pressure over the wing. The magnitude of the force acting over a small section of an object immersed in a fluid equals the pressure p times the area A of the section. A quick units check shows that: p * A = (force/area) * area = force As discussed on the fluid pressure slide, pressure is a scalar quantity related to the momentum of the molecules of a fluid. Since a force is a vector quantity, having both magnitude and direction, we must determine the direction of the pressure force. Pressure acts perpendicular (or normal) to the solid surface of an object. So, the direction of the force on the small section of the object is along the normal to the surface. We denote this direction by the letter n. The normal direction changes from the front of the airfoil to the rear and from the top to the bottom. We indicate this variation on the figure by several small arrows pointing perpendicular to the surface and labeled with an n. To obtain the net mechanical force over the entire solid object, we must sum the contributions from all the small sections. Mathematically, the summation is indicated by the Greek letter sigma ( ) The net aerodynamic force F is equal to the sum of the product of the pressure p times the incremental area delta A in the normal direction n. F =   p * n * delta A In the limit of infinitely small sections, this gives the integral of the pressure times the area around the closed surface. Using the symbol S dA for integration, we have: F = S (p * n) dA where the integral is taken all around the body. On the figure, that is why the integral sign has a circle through it. If the pressure on a closed surface is a constant, there is no net force produced because the summation of the directions of the normal adds up to zero.

Basic Principles of Fluid and Lift 2

F =   p * n * delta A In the limit of infinitely small sections, this gives the integral of the pressure times the area around the closed surface. Using the symbol S dA for integration, we have: F = S (p * n) dA where the integral is taken all around the body. On the figure, that is why the integral sign has a circle through it. If the pressure on a closed surface is a constant, there is no net force produced because the summation of the directions of the normal adds up to zero. For every small section there is another small section whose normal points in exactly the opposite direction. F = S (p * n) dA = p * S n dA = 0 For a fluid in motion, the velocity has different values at different locations around the body. The local pressure is related to the local velocity, so the pressure also varies around the closed surface and a net force is produced. On the figure, at the lower right, we show the variation of the pressure around the airfoil as obtained by a solution of the Euler equations. The blue line shows the variation from front to back on the lower surface, while the red line shows the variation from front to back on the upper surface, The black line gives the reference free stream pressure. Summing the pressure perpendicular to the surface times the area around the body produces a net force. F = S (p * n) dA Definitions of Lift and Drag Since the fluid is in motion, we can define a flow direction along the motion. The component of the net force perpendicular (or normal) to the flow direction is called the lift; the component of the net force along the flow direction is called the drag. These are definitions. In reality, there is a single, net, integrated force caused by the pressure variations along a body. This aerodynamic force acts through the average location of the pressure variation which is called the center of pressure. Velocity Distribution For an ideal fluid with no boundary layers, the surface of an object is a streamline. If the velocity

G Limiter

9 G's or 9 times Earth's gravity.