
Afterburners are used on jet engines to increase thrust, usually during supersonic flight, takeoff, and combat. They are mostly used on military aircraft. Afterburners inject additional fuel into the jet pipe behind the turbine, increasing the velocity of exhaust gas and resulting in a significant increase in engine thrust. However, they are extremely fuel-inefficient and are therefore only used sparingly, such as during takeoffs from short runways or in combat.
| Characteristics | Values |
|---|---|
| Purpose | To increase thrust |
| Use cases | Supersonic flight, takeoff, and combat |
| Mechanism | Injecting additional fuel into a combustor in the jet pipe behind the turbine |
| Result | Increase in engine thrust, fuel consumption, and gas temperature |
| Efficiency | Not very efficient due to high fuel consumption and energy wastage |
| Speed | Can increase speed by 50% or more |
| Use frequency | Used sparingly due to high fuel consumption |
| Engine type | Mostly used on military supersonic aircraft |
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What You'll Learn

The use of afterburners for military jets
Afterburners are mostly used on military jets and fighter jets, and they are considered standard equipment for the latter. They are used to increase thrust, which is necessary for supersonic flight, takeoff, and combat situations. Afterburners are particularly useful for taking off from short runways, such as aircraft carriers, and during high-speed manoeuvres in dogfights. They are also handy for aircraft that need to quickly climb to high altitudes.
The afterburning process involves injecting additional fuel into a combustor ("burner") in the jet pipe behind the turbine, reheating the exhaust gas. This significantly increases thrust without requiring a bigger engine, which would add weight and decrease fuel efficiency. However, the trade-off is that afterburners have high fuel consumption and are inefficient, making them practical only for short periods.
The gas temperature decreases as it passes through the turbine and then the afterburner combustor reheats the gas to a much higher temperature. This results in the gas being accelerated, first by the heat addition, known as Rayleigh flow, and then by the nozzle, which gives it a higher exit velocity. The mass flow is also slightly increased by the addition of afterburner fuel.
The use of afterburners can increase the thrust of a jet engine by 50% or more, providing significantly higher performance without adding much weight or complexity to the engine. This is particularly useful for military jets, which often require sudden bursts of speed and power. However, due to their high fuel consumption, afterburners are generally used sparingly and only when absolutely necessary.
While afterburners are predominantly used in military applications, there have been a small number of civilian planes that have utilised them, including some NASA research aircraft, the Tupolev Tu-144, Concorde, and the White Knight of Scaled Composites.
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Fuel consumption and efficiency
An afterburner is an additional combustion component used on some jet engines, mostly those on military supersonic aircraft. It increases thrust by injecting extra fuel into a combustor in the jet pipe behind the turbine, reheating the exhaust gas. This process increases the afterburner exit temperature, resulting in a significant increase in engine thrust.
The major downside of using an afterburner is its high fuel consumption, making it practical only for short periods. This is because the afterburner significantly increases the velocity of the exhaust gas, which is one of the two main determinants of thrust. The other determinant is the mass of the gas exiting the nozzle.
A jet engine can produce more thrust by either accelerating the gas to a higher velocity or ejecting a greater mass of gas from the engine. Turbofan engines, which produce the latter, are highly fuel-efficient and can deliver high thrust for long periods. However, the trade-off is their large size relative to the power output.
Afterburners are generally used only in military aircraft and are considered standard equipment on fighter jets. They are used for short-duration, high-thrust requirements, such as heavyweight or short-runway take-offs, assisting catapult launches from aircraft carriers, and during air combat.
The high fuel consumption of afterburners means that most planes use them sparingly. For example, a military jet might use its afterburners during a high-speed manoeuvre in a dogfight or when taking off from a short runway.
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Jet engine design
The jet engine has evolved significantly since its early attempts in the form of hybrid designs, which used an external power source to compress air, mix it with fuel, and burn it for jet thrust. The development of the gas turbine engine, the most common form of jet engine, was motivated by the need to surpass the limitations of propeller efficiency. The key to a practical jet engine was the gas turbine, which could extract power from the engine itself to drive the compressor.
One notable pioneer in jet engine design was Whittle, who patented a two-stage axial compressor feeding a single-sided centrifugal compressor in 1932. However, his invention failed to garner government interest, and development progressed slowly. In contrast, von Ohain's axial-flow engine design, which used hydrogen fuel supplied under external pressure, was eventually adopted by most manufacturers by the 1950s.
Today, jet engine design typically focuses on optimising performance by considering two key parameters: specific thrust (ST) and specific fuel consumption (SFC). Turbine designers aim to maximise the turbine inlet temperature (TET) to keep the engine compact while balancing the trade-off between ST and SFC. Increasing TET, for instance, leads to higher SFC, but the gain in ST is often prioritised, especially at high flight speeds where engine size is crucial.
Another important aspect of jet engine design is the choice between different types of engines, including turbojet, turbofan (or bypass engine), turboprop, and turboshaft. The turbofan engine, for example, sacrifices speed for higher fuel efficiency and the ability to deliver high thrust over extended periods. On the other hand, afterburners can be used to temporarily boost thrust by injecting additional fuel into the combustor, although this comes at the cost of significantly increased fuel consumption.
The use of afterburners is therefore limited to short durations, such as during take-off or combat manoeuvres in military jets. The design of a jet engine with an afterburner must include an adjustable nozzle to accommodate both afterburner and non-afterburner operation. While afterburners enhance performance, they also contribute to increased fuel consumption and pollution, making their use a carefully weighed decision in jet engine design.
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Environmental impact
The environmental impact of jet afterburners is significant due to their high fuel consumption and associated emissions. Afterburners are used to increase the thrust of jet engines, typically during take-off, supersonic flight, and combat situations. While they provide a significant boost in power, they do so at the cost of increased fuel usage, which can be up to 8 times that of normal operations. This results in a higher rate of fuel burning, leading to greater emissions of combustion products and pollutants into the atmosphere.
The combustion process in jet engines involves burning fuel with oxygen from the ingested air. Even without afterburners, jet engines only utilize about half of the oxygen they take in, leaving significant untapped potential for power generation. Afterburners take advantage of this by injecting additional fuel into the exhaust stream, where it is burned with the remaining oxygen. This process increases thrust without requiring a larger engine, which would add weight and complexity.
However, the downside of this increased thrust is the significant environmental impact. The high fuel consumption of afterburners leads to a corresponding increase in emissions. These emissions contribute to air pollution and the release of greenhouse gases, particularly carbon dioxide, which is a major driver of climate change. The combustion process also produces other pollutants, such as nitrogen oxides (NOx), which have harmful effects on human health and the environment.
The specific environmental impact of jet afterburners can vary depending on the type of fuel used. For example, the use of kerosene as a fuel contributes to the emission of particulate matter, carbon monoxide, unburned hydrocarbons, and sulfur oxides. These pollutants have detrimental effects on air quality, human health, and the environment, including the formation of smog and acid rain.
Additionally, the high temperatures reached during the afterburning process, upwards of 1,390 °C (2,540 °F), can impact the composition of the emitted pollutants. High combustion temperatures can lead to the formation of more complex and toxic pollutants, such as polycyclic aromatic hydrocarbons (PAHs) and volatile organic compounds (VOCs). These pollutants can have persistent and harmful effects on the environment and human health, including the potential for carcinogenic and mutagenic impacts.
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Alternative methods for increasing thrust
Afterburners are a method of increasing thrust in jet engines, but they come with the drawback of high fuel consumption, making them impractical for extended use. Here are some alternative methods for increasing thrust:
Turbofan Engines: These engines are designed around the principle of ejecting a greater mass of gas from the engine, resulting in higher thrust. Turbofans produce slower gas but in larger quantities, making them highly fuel-efficient. However, the trade-off is their larger size relative to power output.
Duct Heating: This method involves using a duct heater with an annular combustor to increase thrust during takeoff, climb, and cruise. The duct heater augments the engine's performance by burning additional fuel after the gas flow has left the turbines.
Engine Design: Increasing the size of the jet engine is another way to boost thrust. While this approach provides more power, it also increases weight, frontal area, and fuel consumption. As a result, it may not be the most efficient option for short-term thrust augmentation.
Variable Nozzle: Afterburning jet pipes are often equipped with variable nozzles that can open or close to adjust the exit area for the gas stream. This prevents pressure increases in the jet pipe, allowing for operation under various conditions.
Fuel Injection Techniques: Injecting fuel directly into the exhaust stream and burning it using the remaining oxygen can increase thrust. This technique, employed in afterburners, takes advantage of the oxygen available in the exhaust stream of modern turbine engines.
These alternative methods offer different approaches to increasing thrust while managing the challenges of fuel efficiency, engine size, and operational conditions.
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Frequently asked questions
An afterburner is an additional combustion component used on some jet engines, mostly those on military supersonic aircraft. Afterburners inject extra fuel into the jet pipe behind the turbine, which is then ignited, increasing thrust.
Afterburners are highly polluting due to their high fuel consumption, which can be up to 10 times that of normal fuel usage. This results in decreased fuel efficiency and increased emissions.
Afterburners are used sparingly, only when extra thrust is required, such as during take-off, combat, or supersonic flight. They allow for significantly higher performance without adding much weight or complexity to the engine.
Yes, one alternative is to use a larger engine to increase thrust. However, this also increases weight, frontal area, and fuel consumption. Afterburners are therefore the best method for increasing thrust over short periods.







































