Nepedia
Back to Discover
Advanced Reader
💻

Rocket engine

technology Maturity 11-13 Next article →

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
Rocket thrust

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
RS-68 rocket engine test

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
Liquid-Fuel Rocket Diagram

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
Solid-Fuel Rocket Diagram

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
Nozzle de Laval diagram

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
Rocket nozzle expansion

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
Viking 5C rocketengine

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.

707 words

Where will your curiosity go next?

Keep exploring at your chosen reading level.

🖼️ 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
More to explore

🔬 Go deeper

More advanced topics to explore

🪜 Step back

Simpler topics to build understanding

What is Nepedia?

A free, ad-free encyclopedia for children. Every article is written at five reading levels, so the same page works for a five-year-old and a fifteen-year-old — use the level switcher above to see this one change. No account needed to read.