So it is impossible to provide enough oxygen from the air for five rockets to burn fuel at a very fast speed. The most important thing is that the air is diluted to a high level. At the initial altitude of 20,000 feet (the height of Saturn rocket is only 55 times), the air density will drop to 4% of the space, and the oxygen in the air will also drop. Of course, someone will ask the rocket. They can ask about the lack of oxygen in the rocket air. How can a jet plane fly? In terms of efficiency, jet engines have great advantages in launching rockets in space. They can cruise most of the time at any altitude and speed, which is the best compromise between resistance and fuel economy. They don't need to go into space, so they don't need to accelerate to Mach 20 and climb to the oxygen supply. This means that they can take in oxygen at a slow enough speed, and then use the quality of air to promote oxygen.
The famous Rolls-Roystrerent 1000 gas turbine fan generates 285-33 1 rod thrust (64 100-74400), accounting for about 4% of the fixed F- 1 rocket engine. Because of this, it can inhale 1.25 tons (900 cubic meters) of air per second, but only a small part of it is compressed and burned with fuel, and the rest is the reaction mass of engine thrust. Such an engine only needs a jet of 0/5-20 gallons per minute, and it needs about 400-600 gallons of air. It is easy to provide power by sliding and compressor. Unlike rockets, their thrust hardly emits exhaust gas. In contrast, exhaust gas is used to turn a turbine, which drives a large fan, and the fan quickly enters the air.