Does a fighter have a take off weight and a landing weight

Yes, but generally not so, to be precise, the maximum take-off weight and the maximum landing weight. These two are the limit values, and the weight of the fuel and the aircraft itself during take-off cannot exceed the maximum take-off weight, not that it must not be able to fly if it exceeds this value, but that it is easy to have an accident. The maximum landing weight, this is not very easy to say, there is a speed range when landing, that is, your type of aircraft is best to land in which speed range, of course, with**with**with**, more oil and less oil is also different, generally the lighter the better.

Sometimes you will see a white flower spraying from the tail of the fighter, that is, the plane is draining fuel, reducing weight and preparing for landing.

Take-off weight is a performance indicator of an aircraft. If it is exceeded, the plane cannot take off. As for the speed of the descent, it is mainly determined by the speed of descent and the magnitude of the glide angle.

The tactical actions of diving and jumping in battle are determined according to tactical needs. And not the weight. Of course, to descend quickly, the only way to make the plane stall at a large angle of attack is to enter a spiral and descend the fastest.

This is a very dangerous maneuver that can only be done by specially trained people.

The take-off weight of a fighter jet refers to its total external weight, while the take-off weight of a transport aircraft refers to its load capacity! But there is no landing weight, as long as there are no accidents, you can definitely take off.

Absolutely. **Not to mention, even fuel will change!

Nonsense, the fighters are divided into three grades: light, medium and heavy, based on the full take-off weight! The F15 F22 is a heavy machine, the F35 16 is a light machine, and the F18 and Rafale are medium aircraft.

The maximum take-off mass of an aircraft is determined by the engines of the aircraft, and currently the maximum take-off mass of the largest aircraft in the world is 640 tons.

The maximum take-off mass of an aircraft is the maximum weight that an aircraft can tolerate during take-off due to design or operational limitations. The maximum take-off weight is one of the three design weight limits for the aircraft, the other two being the maximum zero fuel weight and the maximum landing weight. The total weight of the aircraft is calculated before the flight.

The pilot calculates the required take-off speed of the aircraft based on the gross weight and ensures that the total weight is below the maximum take-off weight.

The principle of the take-off of an airplane

The aircraft must be able to generate a lift force greater than the gravitational force of the aircraft itself during take-off in order to lift the aircraft off the ground. Since the aircraft can only produce a limited lift, the total weight of the aircraft itself must be limited to ensure that it can take off from the ground normally.

In practical applications, the maximum take-off weight is also limited by other factors, such as runway length, atmospheric temperature, take-off plane pressure altitude and obstacle crossing ability. When determining the maximum approved take-off weight of a civil aircraft, it is necessary to meet certain airworthiness standards, which are generally measured under the international standard atmospheric conditions stipulated by the International Civil Aviation Organization.

1.Ordinary aircraft:

Take off: hold down W to accelerate, press the key when the tail of the plane is raised (that is, the speed has reached a certain level), lift the nose of the aircraft, press the + key of the keypad to retract the landing gear, climb up, do not keep pressing the key, then the plane will fall.

Level flight: Hold down W to accelerate, A and D keys can be steered by tilting the wings (advantages: large amplitude, disadvantages: difficult to control), Q and E are steered by vertical tail (just the opposite of the A and D buttons).

Landing: Press the + key of the keypad to lower the landing gear, press the S key to slow down, then press the key to descend, and then press the button to lift the nose of the aircraft when landing (imagine a real plane landing).

2.Harrier VTOL Fighter:

Take off: Press and hold the W key, it will rise vertically, then press the + key of the keypad to put away the landing gear, press and hold the number key 8 of the keypad, at this time the thruster turns back, pay attention to the W key to hold on, and then you can enjoy the rapid flight

Level flight: Same as "ordinary aircraft".

Hail falls: There are two kinds of landing, one you can do like a normal plane, and the other is: press the S to reduce the speed before landing, press the keypad + lower the landing gear, press the keypad number keys 2 Turn the thruster down, and then press and hold the S key.

: Take off: Press and hold W.

Forward: Press the W key and then press the button in the morning car, and don't hold the upper button unless you want to play Black Hawk Down.

Back: Press and hold the W key and then press the KEY again.

Landing: Press and hold the S key.

Some planes have machine guns, so try pressing the left CTRL key to shoot bullets, the spacebar to aim (green track, turn red to lock), and shift to fire missiles.

Take the planes of the two major aircraft manufacturers that are common in China as an example, and take a look at the weight of the aircraft. First of all, the classic and more common Boeing-737, this series has four models, the approximate fuselage is about 40 tons, the maximum take-off weight is about 80 tons, this is also a relatively small and light model in civil airliners, its flight speed is relatively fast, generally used for short-distance flights.

The same very common Airbus A320 series, this series of aircraft weighs about 40 tons, the maximum take-off weight is basically not more than 80 tons, it is also an aircraft suitable for short-haul flights, and such airliners generally cannot carry too much luggage.

Most aircraft are made up of the following six main parts: wings, fuselage, tail, landing gear, control system, and power plant. Each of them has its own unique function.

The fuselage is mainly used to carry personnel, cargo, fuel, ** and on-board equipment, and through it, the wings, tail, landing gear and other components are connected into a whole. In light aircraft, fighter planes, and attack aircraft, the engine is often installed in the fuselage.

Wings usually have straight wings, swept wings, delta wings, etc. The front and rear green of the wing are basically straight and the leading edge and trailing edge of the wing are swept backward is called the swept wing;

The delta wing is called a delta wing with a triangular plane shape, the former is suitable for low-speed aircraft, and the latter two are suitable for high-speed aircraft. Recently, advanced aircraft have also adopted planar shapes such as edge strip wings and forward-swept wings.

When the aircraft is ascending or descending, the overweight and weightlessness of the people in the aircraft depend on the direction and magnitude of the acceleration of the aircraft.

If the aircraft rises or falls at a constant speed, then the people in the aircraft will be in a situation where they are neither overweight nor weightless.

If the plane accelerates, for example, at an upward acceleration, the people in the plane will be overweight because their gravitational acceleration is upwards and is larger than they would normally feel.

Similarly, if the plane accelerates to descend, for example, with downward acceleration, then the people in the plane will be weightless because their gravitational acceleration is downward and greater than the gravitational force they would normally feel.

In conclusion, whether people are overweight or weightless during the ascent or descent of an aircraft mainly depends on the direction and magnitude of the aircraft's acceleration.

When the aircraft rises at a constant speed, the people in the aircraft are neither overweight nor weightless;

When the plane accelerates upward, the people in the plane are overweight;

When the aircraft slows down and rises, the people in the aircraft are weightless;

When the aircraft descends at a constant speed, the people in the aircraft are neither overweight nor weightless;

When the plane accelerates to descend, the people in the plane are weightless;

When the plane slowed down and fell, the people in the aircraft fluid banquet were overweight.

Overweight bridge brightness occurs when there is upward acceleration, and weightlessness occurs when there is downward acceleration.