Fairchild Republic A-10C Thunderbolt II

Has a 30mm galting gun called the GAU-8/Avenger, it fires 30mm×173mm cartridges at 3,900 Rounds per Minute and is located on the nose of the aircraft.

51,000 Pounds

420 Miles Per Hour or MACH 0.56

Powered by two General Electric TF34-GE-100 Turbofan jet engines that both produce 9,065 pounds of thrust from each engine

16.16 Meters

4.42 Meters

17.42 Meters

13,636 meters or 45,000 feet

800 Miles

Up to 16,000 pounds (7,200 kilograms) of mixed ordnance on eight under-wing and three under-fuselage pylon stations, including 500 pound (225 kilograms) Mk-82 and 2,000 pounds (900 kilograms) Mk-84 series low/high drag bombs, incendiary cluster bombs, combined effects munitions, mine dispensing munitions, AGM-65 Maverick missiles, laser-/GPS-guided bombs, unguided and laser-guided 2.75-inch (6.99 centimeters) rockets; infrared countermeasure flares; electronic countermeasure chaff; jammer pods; illumination flares and AIM-9 Sidewinder missiles.

A dedicated Close Air Support and Foward Air Guidance aircraft

The Modernized C Variant of the A-10 equips it with modern avionics to allow it to use more modern weaponry such as precision bombs like laser guided, and more modern GPS guided bombs. Also better communication and connectivity with other aircraft for datalink.

It is just a plane and bares no consciousness what's so ever also it is parked with no-one inside the cockpit.

General Electric

Produced from 1972-1984 by Fairchild Republic, only 716 of them were built now only 281 serve the United States Airforce

A-10 Warthog, Warthog, Fairchild Republic A-10 Warthog, Thunderbolt 2, Thunderbolt ii, A-10, Fairchild Republic A-10C Thunderbolt II

United States of America

A Straight Wing design with a H-tail design

It can easily be repaired, and can fly on one wing with the right pilot, and a little bit of luck, self-celling fuel cells that are protected by Internal and External Foam that suppresses fires, Can survive direct hits from Armor-Piercing and High Explosive projectiles of up 23mm and with Manual systems backing up their redundant hydraulic flight-control systems, allowing pilots to fly and land when hydraulic power is lost. The pilot and important parts of the flight control system are protected by a 30mm titanium "tub" inside the aircraft.

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 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 = The Greek letter sigma 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 lo