Specific Impulse: Physical Meaning and Rocket Implications

In summary: You could find the design for the X-33 engine on the NASA website, but it's not the only engine that is being developed for the Hyperspace program. There are a number of different engines being developed, including a scramjet.
  • #1
Clausius2
Science Advisor
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What is the physical meaning of the specific impulse?. All i know is what I've read in rocket informations. Its dimensions are s^(-1), and appear as one of the principal variables in rocket engines.

Thanks.
 
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  • #2
I think it means, "The speed and how effeciently the exhaust of a rocket helps you."

The higher the specific impulse, (ISP) the faster you can go. Chemical rockets (ISP = 450) are relatively ineffecient for going to stars, but highly effective for getting off the planet. With the exception of nuclear pulse rockets (ISP = 10,000), acceleration is faster with lower ISP. Thus, an antimatter-matter annihilation rocket will take centuries just to accelerate to near the speed of light, as it's ISP equals around 280,000.

Glad to be of service.
 
  • #3
You're sort of right, LF.

It is the efficiency of the rocket, but it doesn't define top speed. The combination of Isp and the fuel ratio of the rocket determine your final speed.

Specific Impulse is defined as:

[tex] \frac{T}{dm/dt * g_0}[/tex]

where
T is the rocket's thrust
dm/dt is the propellant mass flow
and
g0 is the acceleration of gravity at Earth sea level.

The units are 'seconds', not s-1

The term basically sums up how efficient a rocket engine is. For any specific propellant combination, you can make a different engine which produces more thrust, but the mass flow will increase proportionally.

The theoretical Isp, which is what is listed for propellant combinations is a function of the propellants alone. Actual Isp is lower, and also depends on ambient pressure and the geometry of the expansion nozzle. The actual Isp is what is listed if you're looking at specific motors.

Isp * g0 is also the velocity of the exhaust plume relative to the rocket in units defined by g0
 
  • #4
Semi-mea culpa. *grins*
 
  • #5
Good explanations, guys.
Thanks.
 
  • #6
And congratulations for the record of velocity of the X-33 proyect(is this its name?. I've watched it today on the TV. USA is USA, as we say here.

I could question this in the article of the hypersoar program, but since I'm here now: in which web page i could see the internal design of the X-33? I'm referring to Scramjet engine. I haven't had success in looking for one really good.
 

Related to Specific Impulse: Physical Meaning and Rocket Implications

1. What is specific impulse and why is it important in rocket science?

Specific impulse, also known as Isp, is a measure of the efficiency of a rocket engine. It is defined as the thrust produced by a rocket engine per unit of propellant consumption. In other words, it measures how much thrust a rocket engine can produce using a certain amount of propellant. It is an important concept in rocket science because it helps determine the performance and overall capabilities of a rocket.

2. How is specific impulse related to rocket fuel?

Specific impulse is directly related to the type of rocket fuel being used. Different types of fuel have different energy densities, which affect the specific impulse of a rocket engine. For example, liquid hydrogen has a higher specific impulse compared to kerosene, meaning it can produce more thrust using the same amount of propellant. This is why specific impulse is an important consideration when choosing a rocket fuel for a particular mission.

3. What are the units of specific impulse?

Specific impulse is typically measured in seconds (s) or meters per second (m/s). This is because it represents the change in momentum of the rocket per unit of mass of propellant consumed. In the metric system, specific impulse is measured in seconds, while in the English system, it is measured in seconds per pound (s/lb).

4. How is specific impulse affected by atmospheric conditions?

The specific impulse of a rocket engine is affected by atmospheric conditions, specifically the pressure and temperature of the air surrounding the rocket. As the rocket ascends through the atmosphere, the pressure decreases and the temperature changes, which can affect the performance of the rocket engine. This is why specific impulse is usually measured at a specific altitude and temperature to provide a more accurate representation of its capabilities.

5. Can specific impulse be improved?

Yes, there are various ways to improve the specific impulse of a rocket engine. One way is by using more efficient rocket fuels, such as liquid hydrogen or methane. Another way is by using advanced engine designs, such as staged combustion or turbopumps, which can increase the efficiency of propellant consumption. However, there is a trade-off between specific impulse and other factors such as cost and complexity, so achieving the highest specific impulse may not always be the most practical solution.

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