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Rocket engine

technology Maturity 11-13

A rocket engine is very strong.

RS-68 rocket engine test.jpg
RS-68 rocket engine test.jpg
It pushes hot gas out the back. This push moves the rocket up. It helps ships go to space. It is very fast! Do you want to fly to the stars?

41 words

A rocket engine is very strong.

RS-68 rocket engine test.jpg
RS-68 rocket engine test.jpg
It works by pushing gas out the back. This push moves the rocket forward.

Inside, fuel and air mix and burn. This makes a very hot gas. The gas moves through a narrow part.

Liquid-Fuel Rocket Diagram.svg
Liquid-Fuel Rocket Diagram.svg
Then it goes through a wide nozzle.

The gas moves out at a high speed. This speed is much faster than sound. The push from the gas moves the ship.

Rocket thrust.svg
Rocket thrust.svg

Some rockets use liquid fuel. Others use solid fuel. Rockets can even work in space. Space has no air to breathe.

These engines help ships reach great speeds. They can even help ships leave Earth. It is a very powerful way to fly.

122 words

A rocket engine is a powerful tool. It creates thrust to move ships and missiles.

RS-68 rocket engine test.jpg
RS-68 rocket engine test.jpg
It works by pushing gas out the back. This follows a rule called Newton's third law. This rule says every action has an opposite reaction.

Most engines need air to burn fuel. But rockets carry their own oxidizer. An oxidizer is a substance that helps fuel burn. This lets rockets work in the vacuum of space.

Liquid-Fuel Rocket Diagram.svg
Liquid-Fuel Rocket Diagram.svg
There are different ways to make them work. Some use liquid fuel. These use pumps to move fuel into a chamber.
Solid-Fuel Rocket Diagram.svg
Solid-Fuel Rocket Diagram.svg
Other rockets use solid fuel. This fuel is a hard mix called grain.

Inside the engine, fuel and oxidizer mix and burn. This makes hot, high-pressure gas. The gas travels through a narrow throat. Then it enters a wide nozzle.

Rocket nozzle expansion.svg
Rocket nozzle expansion.svg
This shape is called a de Laval nozzle. The nozzle makes the gas move at very high speeds. Some gas moves ten times faster than the speed of sound! This fast gas pushes the rocket forward.

181 words

A rocket engine is a special kind of reaction engine. It produces thrust, which is the push that moves a vehicle forward. This works because of Newton's third law. This law says that for every action, there is an equal and opposite reaction.

RS-68 rocket engine test.jpg
RS-68 rocket engine test.jpg
Rockets push mass, like hot gas, out the back very quickly. This push sends the rocket in the opposite direction. Because they carry their own oxidizer, rockets can work in the vacuum of space. Most other engines need to breathe air to burn fuel.
Liquid-Fuel Rocket Diagram.svg
Liquid-Fuel Rocket Diagram.svg

How does the engine actually work? First, the engine must mix fuel with an oxidizer. This happens inside a part called a combustion chamber. In liquid-propellant rockets, pumps feed the liquids from tanks into the chamber.

Solid-Fuel Rocket Diagram.svg
Solid-Fuel Rocket Diagram.svg
Once they mix, they undergo a chemical reaction that creates intense heat and pressure. This creates a high-speed jet of hot gas. The gas then travels through a narrow space called a throat. As the gas moves through the nozzle, it reaches supersonic speeds. This means it travels faster than the speed of sound.
Nozzle de Laval diagram.svg
Nozzle de Laval diagram.svg

Scientists and engineers have studied many ways to power these engines. Chemical rockets are the most common type used today. Some use solid fuel, which is a hard mixture called grain. Others use liquid fuel, which can be more complex to manage. There are even hybrid rockets that use both solid and liquid parts. Some rockets use a single propellant that is broken down by a catalyst. This is called a monopropellant rocket. These different methods allow rockets to perform many different jobs.

Viking 5C rocketengine.jpg
Viking 5C rocketengine.jpg

There are many important numbers and facts about these engines. A common nozzle shape is called a de Laval nozzle. It has a wide bell shape to help the gas expand. This expansion can make gas move ten times faster than the speed of sound. Engineers look at a number called the characteristic length to design the chamber. This number is the volume of the chamber divided by the area of the throat. In space, the pressure is almost zero. This is very different from the high pressure found at sea level.

Rocket nozzle expansion.svg
Rocket nozzle expansion.svg

You can think of a rocket engine like a balloon. If you blow up a balloon and let it go, the air rushes out. The air pushing out one way makes the balloon fly the other way. Rocket engines do this on a much larger and more powerful scale. They use massive amounts of energy to reach great speeds. This allows them to reach escape velocity to leave Earth.

Rocket thrust.svg
Rocket thrust.svg
Without these engines, we could not send spaceships into the stars.

454 words

A rocket engine is a type of reaction engine designed to produce thrust. This thrust is the force that moves a vehicle forward. Engines follow Newton's third law of motion. This law states that for every action, there is an equal and opposite reaction.

Rocket thrust.svg
Rocket thrust.svg
To create this movement, the engine ejects a reaction mass rearward. This mass is usually a high-speed jet of hot gas. Unlike jet engines, rockets carry their own oxidizer. This means they can function in the vacuum of space. Because of this, they can reach incredible speeds. They can even reach escape velocity if they have enough delta V.
RS-68 rocket engine test.jpg
RS-68 rocket engine test.jpg

The mechanism of a chemical rocket begins with the propellant. Propellant is the mass stored in tanks or the combustion chamber. In liquid-propellant rockets, fuel and oxidizer are stored separately. These are fed into the combustion chamber by pumps. Sometimes, the system uses tank pressure to move the fluid. For example, the SpaceX Starship uses an autogenous pressurization system. This means it uses gas from the engine cycle to pressurize its own tanks.

Liquid-Fuel Rocket Diagram.svg
Liquid-Fuel Rocket Diagram.svg
Inside the chamber, injectors introduce the propellants. These injectors may be simple holes or complex spray nozzles. They often cause the fluids to collide. This collision breaks the flow into tiny droplets. Smaller droplets burn much more easily.

Once the propellants mix, they undergo an exothermic reaction. This is a chemical reaction that releases heat. This process happens inside the combustion chamber. The chamber is usually a cylinder. The size of this cylinder is very important for efficiency. Engineers use a value called the characteristic length, or L*. This is the volume of the chamber divided by the area of the nozzle throat. L* is typically between 0.5 and 1.5 meters. The temperatures and pressures inside are extreme. Because there is no atmospheric nitrogen to cool the mix, the reaction reaches a true stoichiometric ratio.

Solid-Fuel Rocket Diagram.svg
Solid-Fuel Rocket Diagram.svg

After combustion, the hot gas must be managed by a nozzle. The most common design is the de Laval nozzle. This nozzle has a narrow part called a throat. As gas passes through the throat, it reaches Mach 1. This is the speed of sound. The gas then enters a diverging expansion section. Here, the gas continues to accelerate to supersonic speeds. This process converts thermal energy into kinetic energy. Exhaust speeds can reach ten times the speed of sound at sea level.

Nozzle de Laval diagram.svg
Nozzle de Laval diagram.svg
About half of the thrust comes from chamber pressure. The other half comes from pressure acting against the nozzle walls.

Engineers must consider how the nozzle interacts with the atmosphere. This is known as the expansion regime. A nozzle is perfectly expanded when the exit pressure equals the ambient pressure. If the exit pressure is higher, it is under-expanded. If the exit pressure is lower, it is over-expanded.

Rocket nozzle expansion.svg
Rocket nozzle expansion.svg
An over-expanded nozzle can cause shock diamonds to form. In extreme cases, a shock wave forms inside the nozzle. This is called a grossly over-expanded nozzle. This can cause mechanical problems or side forces. These forces can make the rocket difficult to control. To fix this, scientists propose designs like the aerospike or plug nozzle. These help the engine adapt to changing air pressure.

There are several distinct types of rocket engines. Chemical rockets are the most common. These include solid-fuel rockets, which use a solid mixture called grain. They also include hybrid rockets. A hybrid rocket uses a solid fuel with a liquid or gaseous oxidizer. There are also monopropellant rockets. These use a single propellant that is decomposed by a catalyst. Common examples include hydrazine and hydrogen peroxide. Other types include thermal rockets. These use an inert propellant heated by electricity or a nuclear reactor.

Viking 5C rocketengine.jpg
Viking 5C rocketengine.jpg
Nuclear thermal rockets have high efficiency but low thrust.

Rocket engines are essential for many different vehicles. They power missiles, artillery shells, and ballistic missiles. Most importantly, they propel spaceships. While they provide the highest thrust, they are often propellant-inefficient. This efficiency is measured by specific impulse. Pure hydrogen provides the highest exhaust velocity because it is the lightest element. However, most practical rockets use heavier mixtures. This reduces the overall exhaust velocity. Despite these trade-offs, rocket engines remain the primary way we explore the cosmos.

717 words
🖼️ Images & Media (9)
File:RS-68 rocket engine test.jpg
RS-68 rocket engine test.jpg
File:Viking 5C rocketengine.jpg
Viking 5C rocketengine.jpg
File:Liquid-Fuel Rocket Diagram.svg
Liquid-Fuel Rocket Diagram.svg
File:Solid-Fuel Rocket Diagram.svg
Solid-Fuel Rocket Diagram.svg
File:Rocket thrust.svg
Rocket thrust.svg
File:Rocket nozzle expansion.svg
Rocket nozzle expansion.svg
File:Nozzle de Laval diagram.svg
Nozzle de Laval diagram.svg
File:Rocket propulsion efficiency.svg
Rocket propulsion efficiency.svg
File:Armadillo Aerospace Pixel Hover.jpg
Armadillo Aerospace Pixel Hover.jpg
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