What is the formula to find specific impulse?

The specific impulse formula is Isp = F / (ṁ × g) , the unit of Isp = 1 N/((kg/s) × (m/s²)) = 1 N/(kg⋅m/s³) . But since 1 N = kg⋅m/s² , the units of specific impulse becomes (1 kg⋅m/s²) / (kg⋅m/s³) = s .

What is equivalent velocity?

Where ueq is called the “equivalent exhaust velocity” and is defined as: The first portion of that last equation deals with the pressure field. Basically, it is the exhaust pressure at the end of the nozzle, Pe, minus the ambient pressure outside, Pa, times the exit area of the nozzle, Ae.

What does specific impulse represent?

Specific impulse (usually abbreviated Isp) is a measure of how efficiently a reaction mass engine (a rocket using propellant or a jet engine using fuel) creates thrust.

What is total impulse?

Total impulse is the product of thrust times duration over the motor burn time, and is measured in Newton-seconds (Ns). This measures the total amount of momentum imparted to the rocket by the motor.

How do you calculate delta V?

The following formula is used to calculate the delta-v of a rocket:

  1. ∆v = Ve * ln(mi / mf)
  2. Definition:
  3. Example:
  4. ∆v = Ve * ln(mi / mf)
  5. ∆v = 500 * ln(1000 /400)
  6. ∆v = 458.14 m/s.

How do I calculate thrust?

The force (thrust) is equal to the exit mass flow rate times the exit velocity minus the free stream mass flow rate times the free stream velocity.

What is ISP KSP?

From Kerbal Space Program Wiki. The specific impulse (usually written as Isp, or in-game as ISP) defines the efficiency of an engine. It is thrust per the rate of fuel consumption. Or equivalently, it is change in momentum per amount of fuel consumed.

How fast is rocket exhaust?

For the best chemical rockets, the exhaust speed is around 3,000 meters per second. When electric propulsion is used, exhaust speeds can be up to 20,000 meters per second or more.

Is high specific impulse good?

The engine with the higher value of specific impulse is more efficient because it produces more thrust for the same amount of propellant.

How does specific impulse affect a rocket?

The specific impulse of a rocket propellant is a rough measure of how fast the propellant is ejected out of the back of the rocket. A rocket with a high specific impulse doesn’t need as much fuel as a rocket with low specific impulse. The higher the specific impulse, the more push you get for the fuel that rushes out.

What is the difference between specific impulse and total impulse?

Since Total Impulse is obtained by multiplying thrust by time, the units are pound-seconds (lb-sec.), when English units are used, or Newton-seconds (N-s) when SI units are used. The delivered Specific Impulse (Isp) of the propellant is simply the Total Impulse divided by the propellant weight or mass.

How do you calculate impulse from a graph?

Impulse is the area under the curve of the force vs. time graph. Areas above the time axis are positive Δ p \Delta p Δp and areas below the axis are negative Δ p \Delta p Δp . If the force is not constant, we can divide the graph into sections and add up the impulse in each section.

What is a specific impulse?

From the aforementioned definition, it’s quite evident that you are most likely to hear the term ‘specific impulse’ in conversations regarding rocket and jet engines, especially those that revolve around rocket launches. People often confuse specific impulse with thrust, which are actually two very dissimilar entities.

What is the specific impulse of a propulsion system?

The specific impulse (commonly abbreviated Isp) of a propulsion system is the impulse (change in momentum) per unit of propellant . Depending on whether the amount of propellant is expressed in mass or in weight (by convention weight on the Earth) the dimension of specific impulse is that of speed or time, respectively,…

How do you calculate specific impulse per unit weight?

For all vehicles specific impulse (impulse per unit weight-on-Earth of propellant) in seconds can be defined by the following equation: is the mass flow rate, which is minus the time-rate of change of the vehicle’s mass, since fuel is being expelled.