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—the Saturn v had two stages both parts would burn its engines until the fuel ran out then it would come off the rocket
The rocket carries its own supply of oxygen with which to burn the fuel.
2000 tons of rocket fuel is equal to about 530,000 American gallons. This is the amount of fuel that was aboard the Apollo - Saturn V rocket.
The fuel was liquid oxygen and liquid hydrogen.
A device that ignites the fuel & oxidizer mixture in the rocket engine when a "burn" is to begin.it lights the rocket.
air
it used liquid oxygen
You only have a few choices: -- reduce the total weight (mass) of the rocket and its payload -- burn fuel faster -- burn fuel at the same rate but use fuel with a greater specific impulse
oxygen is added from a separate tank
A rocket motor (rocket engine) does not need air from the atmosphere. It carries the oxidant (source of oxygen) as well as the fuel.
The correct term is "solid propellant rocket". These are rockets that burn fuel that is not a liquid(or they are NOT liquid fuel rockets). These rockets have a fuel that is poured into the rocket case and turns to a solid. Once ignited, there is no stopping the burn or controlling it.A simple example of this is rocket you shoot on the 4th of July. It burns black powder that has been formed into a cardboard case.Whereas, a liquid fuel rocket can be controlled by varying the amount of fuel that is injected into the rocket motor.
I don"t know about the space shuttles but the fuel consumption of the Saturn V"s used in the manned Moon shots was humungous- bear in mind this is various types of rocket fuel, not anything you would find at a service station, but in the initial stage burns the Saturn V consumed- l6 tons of rocket fuel a second! that"s an average fully loaded Truck of the Mack type- 32,000 lbs, in one second!