It is not so difficult to prepare a model of any apparatus if you have mastered the principle of its operation well, you know the design and the relationship of all individual parts. To do this, it is enough just to reduce the size of each block by the same number of times. And in order to more easily understand the principle of a launch vehicle (PA) for launching a UFO, it is even useful to first increase the size of its model to an imaginary natural scale. This consideration determined the methodology for presenting my advice. So, get ready to listen to me carefully, mobilize all your imagination. Imagine that you are in a mountainous area. Pick up two adjacent vertices A and B, the higher the better. After all, PA will be installed on them, and at high altitudes, air resistance to any movement is reduced. On a road that looks like a railroadyou will have a massive blank rolling from A to B and back. Its mass, for example, may be 20 thousand tons. This will be our “working blank” (RB). Let the RB at the initial moment be at the top A. If the depth of the saddle is 2 km, then the potential energy of the RB at any of the top will be 40 billion kgm. Such energy could be obtained by burning 100 tons of liquid fuel. Click on the image to enlarge.
In the absence of friction and energy consumption for spinning the PA, in the depth of the saddle the RB would develop a speed of 200 m / s, which corresponds to a power of 50 million horsepower. In this case, it would take off without assistance to the top B. In reality, its speed will be much lower, and it will stop before reaching the top B. You will have to use a small electric motor and pulley blocks to pull it to the top B. Electric current for engine will give us a small hydroelectric station on a nearby waterfall. It turns out that practically all the energy of the RB will be gravitational. You will not have to burn expensive fuel, or release its combustion products into the atmosphere. How now to transfer part of the energy from RB to PA? RB, falling down, should pull a steel cable wound on the main vertical shaft (GVV) PA. If the RB speed in the lower position is, for example, 20 m / s, and the GWV diameter is 1 m, then the shaft will start rotating at a speed of 6 rev / s. The gear wheels will help to transfer the rotation of the GWV to a parallel (driven) vertical shaft (BBB) with a flying saucer (LT) mounted on it. The figure shows one LT, but several similar BBBs can be installed (according to the number of launched LT). It is desirable, however, that this number be even to ensure a symmetrical load on the hot water supply. If the diameter of the LT is 30 m, then the number of revolutions of the BBB is sufficient to increase to 20 rev / s. In this case, the linear velocity at the edge of the saucer is 2 km / s. Its further increase would lead to significant overheating. The gear wheels will help to transfer the rotation of the GWV to a parallel (driven) vertical shaft (BBB) with a flying saucer (LT) mounted on it. The figure shows one LT, but several similar BBBs can be installed (according to the number of launched LT). It is desirable, however, that this number be even to ensure a symmetrical load on the hot water supply. If the diameter of the LT is 30 m, then the number of revolutions of the BBB is sufficient to increase to 20 rev / s. In this case, the linear velocity at the edge of the saucer is 2 km / s. Its further increase would lead to significant overheating. The gear wheels will help to transfer the rotation of the GWV to a parallel (driven) vertical shaft (BBB) with a flying saucer (LT) mounted on it. The figure shows one LT, but several similar BBBs can be installed (according to the number of launched LT). It is desirable, however, that this number be even to ensure a symmetrical load on the hot water supply. If the diameter of the LT is 30 m, then the number of revolutions of the BBB is sufficient to increase to 20 rev / s. In this case, the linear velocity at the edge of the saucer is 2 km / s. Its further increase would lead to significant overheating.then the number of revolutions of the BBB is sufficient to increase to 20 rev / s. In this case, the linear velocity at the edge of the saucer is 2 km / s. Its further increase would lead to significant overheating.then the number of revolutions of the BBB is sufficient to increase to 20 rev / s. In this case, the linear velocity at the edge of the saucer is 2 km / s. Its further increase would lead to significant overheating.
Passenger and cargo cabins (PCs) should be placed in the central part of the LT. This entire block should be in the form of a cylinder with autonomous rotation about the main axis of the LT. He should not be involved in the rotational movement of the LT at a breakneck speed. But a small rotation with reasonable overload is quite acceptable. These reasonable limits are most reliably determined empirically. Divide the cargo-passenger block into four classes of cabins located at different distances from the axis of rotation, and place one monkey in each "class". The monkeys, of course, need to be equipped with devices by which you can recognize the health and life expectancy of monkeys in different conditions. In the cabin that belongs to the most unlucky animal, assign IV class and in the future use this cabin only for luggage. Just in case, try to make the monkeys look like aliens by putting on silver overalls, fancy helmets, masks, etc. What force will move the LT and control their flight? I answer. With all the simplicity of its design, the absence of signs of any engine, the refusal to burn thermal fuel, your LT will be an amazing combination of a helicopter, a jet plane and a parachute. The helicopter principle, apparently, can be used up to an altitude of 30 km, and higher it will be necessary to switch to jet thrust. When landing, the LT will act as a parachute.refusing to burn thermal fuel, your LT will be an amazing combination of a helicopter, a jet plane and a parachute. The helicopter principle, apparently, can be used up to an altitude of 30 km, and higher it will be necessary to switch to jet thrust. When landing, the LT will act as a parachute.refusing to burn thermal fuel, your LT will be an amazing combination of a helicopter, a jet plane and a parachute. The helicopter principle, apparently, can be used up to an altitude of 30 km, and higher it will be necessary to switch to jet thrust. When landing, the LT will act as a parachute.
The entire internal space of the LT (with a volume of about 2 thousand m ') should be occupied by reservoirs for compressed air (BP), divided into many communicating cells. If the pressure in the tanks is increased to 100 atm, then the total mass of compressed air will be about 200 tons. Air injection into the tanks can be carried out using a system of L-shaped air intake pipes located along the perimeter of the tray. It is necessary to direct one section of it (air intake nozzle) tangentially to the LT (in the direction of rotation of the LT), and the other to the central axial tube (COT), which has four outlets. These exits should be closed off with taps - top (KB), bottom (KN) and two side (KB). Flying into the air intake nozzle at a speed of 2 km / s, highly compressed air enters the central pipe, and from there into the reservoirs, if the KB are open and the KB and KH are closed. If the pressure in the tanks reaches the desired level, and the LT unwinding continues (the RB has not yet dropped to the lower saddle point), then the HF can be opened for a short time. Flying upward, the air will create a reactive force, pressing the plate to the Earth. When the smokeless "gravitational fuel" is completely consumed, then the KB closes and the SC gradually opens, moreover, slowly enough so as not to cause a dangerous overload (the reactive lift from the air rushing down can exceed the weight of the LT by several times). Continuing axial rotation by inertia, the saucer, like a helicopter, will begin to rise up. I think that with a good aerodynamic profile, it can reach an altitude of 30 km. The rotation will not go out there yet, but the rarefied air will no longer be able to create a lifting force to maintain the initial weight of the LT. We'll have to lighten the plate by about 10 tons by releasing compressed air. At the same time, releasing air through the KN, you create additional jet thrust. If the KN has a steering device, then it will give the LT a horizontal speed. By repeating the operation of dumping ballast several times, you will be able to rise to an altitude of 100 km and fly in the chosen direction. Use the rest of the ballast when the LT starts to lose altitude. So you can hold out in the stratosphere, making several flights around the Earth. Save the last portion of ballast for a soft landing (if the parachuting properties of the LT fail). When hot compressed air is released at an altitude of 100 km into an almost complete void, it will almost instantly expand and be dramatically supercooled. Frost particles can form in it, its atoms begin to emit excess energy. The resulting cloud will glow, resembling auroras, noctilucent clouds, rainbows, etc. The cloud will take on a spherical shape. If at an altitude of 100 km it will be 10 km in diameter, then each of you may think that its diameter is 30 m and it is at an altitude of 300 m. Tearing off from the LT, this cloud will float in the stratosphere for a long time, retaining its visible dimensions because its flared edges will gradually fade away for the observer.because its flared edges will gradually disappear for the observer.because its flared edges will gradually disappear for the observer.