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Specific impulse facts for kids

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Estes
A picture showing the force from an Estes A10-PT rocket motor over about 1 second. It also shows the impulse, fuel amount, and specific impulse.

Specific impulse, often called Isp, tells us how good a rocket or jet engine is at using its fuel. It helps us compare different engines, even if they are different sizes. Think of it like "miles per gallon" for a car. A higher specific impulse means the engine uses less fuel to do the same job. This means the rocket can go faster or farther with the same amount of fuel.

A rocket engine with a high specific impulse isn't always the most powerful. For example, ion engines have very high specific impulse but produce very little thrust (pushing force). They accelerate a rocket slowly but steadily over a long time, using tiny amounts of fuel. If two rockets had the same amount of fuel, the one with a more powerful engine would start faster. But the rocket with higher specific impulse would use its fuel more efficiently and keep accelerating for longer. Over a long distance, it would eventually go faster and farther.

How Specific Impulse is Measured

People figure out specific impulse in two main ways. You find it by dividing the impulse by the amount of fuel used. Impulse measures how much force a rocket motor makes and for how long. A motor that makes a small force for a long time can sometimes have a higher impulse than one that makes a big force for a short time. Impulse is measured in Newton-seconds (N·s).

The amount of fuel can be measured in different ways. Sometimes it's measured by its mass (how much "stuff" is in it). When measured by mass, specific impulse is given as a speed, usually in meters per second (m/s). This is also called the effective exhaust velocity. The other way to measure fuel is by its weight (how hard gravity pulls on it). If weight is used, specific impulse is given in units of time, usually in seconds. Both ways are common and help compare how well engines perform.

When the specific impulse is higher, the engine needs less fuel to make the rocket perform well. So, a higher specific impulse means the fuel is used more efficiently.

It's important not to mix up specific impulse with thrust. Thrust is just the force a rocket makes at one moment. Specific impulse measures that force based on how much fuel is used.

When specific impulse is calculated, only the fuel inside the rocket before it fires is counted. This includes both the fuel itself and the oxidizer. The oxidizer is a substance that helps the fuel burn. It can be oxygen or other chemicals.

Examples of Specific Impulse

Specific impulse of different ways to push a rocket
Engine Effective exhaust velocity
(m/s, kg·m/s/kg)
Specific impulse
(s)
Energy per kg of exhaust
(MJ/kg)
Turbofan jet engine
(actual V is ~300)
29,000 3,000 ~0.05    
Solid fuel rocket 2,500 250 3    
Liquid fuel rocket 4,400 450 9.7    
Ion thruster 29,000 3,000 430    
Dual Stage Four Grid Electrostatic Ion Thruster 210,000 21,400 22,500    
VASIMR 30,000-120,000 3,000-12,000 1,400    


Jet engines, like those on airplanes, use fuel better than rocket engines. This is because the gases don't escape as fast. Since they don't escape as fast, the exhaust carries away less energy. This means the jet engine uses much less energy to push the plane. Also, the air that goes through the engine as the jet flies helps the fuel burn faster.

Model Rocket Engines

Specific impulse is also used for model rocket motors. The table below shows some specific impulse values for motors made by Estes. Estes Industries is a well-known American company that sells model rockets. Model rocket motors often have lower specific impulse values than larger rocket engines. This is because they use black powder as fuel, which costs less.

Specific impulses for several Estes rocket motors.
Engine Total Impulse (Ns) Fuel Weight (N) Specific Impulse (s)
Estes A10-3T 2.5 .0370 67.49
Estes A8-3 2.5 .0306 81.76
Estes B4-2 5.0 .0816 61.25
Estes B6-4 5.0 .0612 81.76
Estes C6-3 10 .1223 81.76
Estes C11-5 10 .1078 92.76
Estes D12-3 20 .2443 81.86
Estes E9-6 30 .3508 85.51

Large Rocket Engines

Here are some example numbers for larger rocket engines:

Specific impulse and effective exhaust velocity numbers for a few larger rocket engines.
Engine type Example Use Specific impulse (s) Effective exhaust velocity (m/s)
NK-33 rocket engine Vacuum 331 3,240
SSME rocket engine Space shuttle vacuum 453 4,423
Ramjet Mach 1 800 7,877
J-58 turbojet SR-71 at Mach 3.2 (Wet) 1,900 18,587
Rolls-Royce/Snecma Olympus 593 Concorde Mach 2 cruise (Dry) 3,012 29,553
CF6-80C2B1F turbofan Boeing 747-400 cruise 5,950 58,400
General Electric CF6 turbofan Sea level 11,700 115,000


Units of Measurement

English and SI (Metric system) units for various rocket motor performance measurements.

Specific Impulse
(by weight)

Specific Impulse
(by mass)

Effective exhaust velocity
Specific fuel consumption
SI =X seconds =9.8066 X N•s/kg =9.8066 X m/s =(101,972/X) g/kN•s
English units =X seconds =X lbf•s/lb =32.16 X ft/s =(3,600/X) lb/lbf•h

Today, the most common way to measure specific impulse is in seconds. This unit is used everywhere, whether people use the metric system (SI) or English units. This means you can easily compare engine performance no matter where you are. Most companies that make rocket or jet engines use seconds to show how well their products perform.

Another common way to measure specific impulse is in meters per second (m/s). This is also called effective exhaust velocity. For many engines, the effective exhaust velocity is different from the actual speed at which the gases leave the nozzle.

Related Pages

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See also

Kids robot.svg In Spanish: Impulso específico para niños

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