Liquid oxygen and liquid hydrogen are used as the propellant in the high efficiency main engines of the Space Shuttle. LOX/LH2 also powered the upper stages of the Saturn V and Saturn 1B rockets. Another cryogenic fuel with desirable properties for space propulsion systems is liquid methane.
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The fuel in rockets varies depending on the type of rocket, but commonly used fuels include liquid hydrogen, liquid oxygen, kerosene, and solid propellants such as ammonium perchlorate. These fuels are ignited and combusted to generate the thrust needed for the rocket to lift off and travel through space.
As we know that rocket needs very high energy. So, in rocket liquid hydrogen or hydrogen peroxide is used. chemical formula of hydrogen peroxide is H2O2.
Methane is also used as the fuel in the rocket.Most rockets contain two separate substances : a fuel (hydrogen, kerosene) and an oxidizer (peroxide, tetroxide, or liquid oxygen).
Space Shuttle
The current rockets for the Space Shuttle are of two types.
There are many types of fuel used in rockets. Common ones include kerosene, thermite, hydrazine, and xenon gas.
The two main types of rockets are liquid fuel rockets, which use liquid propellants like liquid oxygen and kerosene, and solid fuel rockets, which use a solid mixture of fuel and oxidizer. Liquid fuel rockets offer more control and efficiency, while solid fuel rockets are simpler in design and more reliable.
Three main types of rockets that power modern spacecrafts are liquid-propellant rockets, solid-propellant rockets, and hybrid rockets. Liquid-propellant rockets use liquid fuel and oxidizer, solid-propellant rockets use solid fuel and oxidizer mixed together, and hybrid rockets use a combination of solid and liquid propellants.
Some rockets, such as liquid fuel rockets, carry liquid oxygen (LOX) as an oxidizer in a separate tank. The LOX is then mixed with the rocket's fuel and ignited to create thrust. Other rockets, like solid fuel rockets, have an oxidizer mixed into their solid fuel composition.
Rockets commonly run on liquid fuel, solid fuel, or a combination of both. Liquid fuel rockets use liquid oxygen and liquid hydrogen, while solid fuel rockets use a solid propellant mixture. Both types of rockets generate thrust through a controlled combustion process.
Solid fuel rockets use a solid propellant mixture, which is more stable and easier to store compared to liquid fuel rockets that use liquid propellants. Iron rockets typically refer to solid fuel rockets using iron particles as part of the propellant mixture to enhance thrust. Overall, solid fuel rockets are simpler and more reliable but lack the efficiency and flexibility of liquid fuel rockets.