There are two types of rockets -- those that use liquid fuel and those that use solid fuel.
Liquid fuel rockets have two main advantages. Liquid fuel rocket engines burning can be controlled. That is, they can be turned on and off, and their thrust (pushing force) can be controlled/varied. Second, they produce more thrust for the same amount (weight) of fuel -- called specific impulse.
Liquid fuel is also cheaper, but that's rarely a consideration as it is such a small part of the cost.
Rocket engines can vary, but some common types include liquid fuel engines (using liquid fuel and oxidizer) and solid fuel engines (using a solid propellant). Each type has its own advantages and disadvantages, based on factors like thrust, efficiency, and complexity.
Liquid rocket engines would act much like a car engine. More fuel, more thrust. Solid rocket engines are either on or off. No throttle control.
Rockets primarily use liquid hydrogen and liquid oxygen as fuel. These are combined in the rocket's engines to produce thrust by undergoing a chemical reaction and creating high-pressure gases that are expelled through a nozzle to propel the rocket forward.
Space Shuttle Main Engines (SSME) are Rocketdyne RS-24 liquid-fuel rocket engines powered by liquid hydrogen and liquid oxygen. The Solid Rocket Boosters used during ascent are solid fuel rockets manufactured by Thiokol Corporation fueled by a mixture of ammonium perchlorate oxidizer, aluminum, an iron oxide catalyst and polymers as a binding agent.
Answer The Space Shuttle is a rocket. By definition, a Rocket is a vehicle that burns gas that it carries with it. Where as, a jet airplane burns the oxygen from the air and is not a rocket. The Rocket when it is launched has a liquid fuel rocket engines at the back end of it. It also has two long, solid fuel rocket engines that separate after launch. But the space shuttle is pulled by a rocket.
The two main types of rocket engines are Solid fuel rocket engines and Liquid fuel rocket engines.
AMMONIA
it bad
Liquid hydrogen is a common fuel used in rocket engines.
Liquid-powered rocket engines have several advantages. Liquid rocket engines have higher specific impulses (Meaning they produce a high amount of thrust for a small amount of fuel) which makes them more efficient. Liquid-powered engines can be throttled in real-time, and have a good control of mixture ratio. They can be shut down and restarted at any time. Liquid rocket engines can be tested before use to ensure that they will operate properly. Liquid engines, such as the Space Shuttle Main Engines (SSMEs), can also be re-used. Because of these safety and performance advantages, liquid engines are commonly used for manned spaceflight. Rocketry pioneer Wernher von Braun even went as far as saying that liquid-fueled engines were the only engines safe to use on manned spacecraft.
gasoline along with liquid oxygen, so the fuel can burn
Less complexity and cost compared to liquid fuel and it's complex, expensive engines
The space shuttle main engines (SSME) RS 24 engines use rocketdyne liquid hydrogen and liquid oxygen fuel in the engine that is designed in such a way that the engines are reusable.
There are two main types of rocket engines: Solid fuel and liquid fuel. Liquid fuel rocket engines are usually considered significantly better than solid propulsion units, however, they are also significantly more expensive.
Rocket engines can vary, but some common types include liquid fuel engines (using liquid fuel and oxidizer) and solid fuel engines (using a solid propellant). Each type has its own advantages and disadvantages, based on factors like thrust, efficiency, and complexity.
liquid fuel
Liquid rocket engines would act much like a car engine. More fuel, more thrust. Solid rocket engines are either on or off. No throttle control.