SOLVED: A rocket with a mass ratio(MR) of 15a change in velocity of 8 km/s,and produces a thrust of 200,000 N.Calculate the specific impulse lsp (2024)

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    SOLVED: A rocket with a mass ratio(MR) of 15a change in velocity of 8 km/s,and produces a thrust of 200,000 N.Calculate the specific impulse lsp (2024)

    FAQs

    How to calculate the impulse of a rocket? ›

    The specific impulse, Isp, with dimensional units of seconds, is the total impulse divided by the amount of propellant that produced that amount of impulse. It is also the ratio of the thrust to the propellant flow rate, I sp = F / m . .

    How to calculate exhaust velocity from specific impulses? ›

    1. Thrust = Isp * g * mass_flow.
    2. Isp is the thrust per weight flow as in pounds thrust per pound flow. Isp * g is also the exhaust velocity. ...
    3. The unit for Isp is seconds. ...
    4. If you know the thrust of the engine and the Isp, you can easily calculate the mass flow rate.
    Jan 8, 2018

    How to calculate theoretical Isp? ›

    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 the specific impulse of 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.

    How to calculate the thrust of a rocket? ›

    Thrust: Thrust is the force that drives the rocket forward and is equal to the rate at which the rocket expels its propellant. It is calculated as the mass flow rate of the propellant multiplied by its exhaust velocity: Thrust = Mass Flow Rate * Exhaust Velocity.

    What is the formula for total impulse? ›

    Total Impulse is found by summing up all the measured thrust values and multiplying this by the time increment.

    What is the formula for impulse from velocity? ›

    By using momentum change: The formula to calculate impulse through momentum change is by calculating the mass of the body and the velocity. In this case, Impulse will be equal to the product of mass and velocity. So J= m*v. Here v will be calculated by subtracting the final velocity from the initial velocity.

    What is the equation for the exhaust velocity of a rocket? ›

    a = v e m Δ m Δ t − g . The greater the exhaust velocity of the gases, the greater the acceleration. The faster the rocket burns its fuel, the greater its acceleration. The smaller the rocket's mass, the greater the acceleration.

    What is the thrust coefficient? ›

    : the thrust force of a jet-propulsion engine per unit of frontal area per unit of incompressible dynamic pressure.

    What is the equation for the ideal rocket? ›

    Δ v = u ln ( m i m ) . This result is called the rocket equation. It was originally derived by the Soviet physicist Konstantin Tsiolkovsky in 1897. It gives us the change of velocity that the rocket obtains from burning a mass of fuel that decreases the total rocket mass from m0 down to m.

    How to calculate thrust impulse? ›

    To calculate the thrust I take the product of mass flow rate and exhaust velocity. This gives 7000*280=1,960,000lbf. Dividing this by 280*32.174 (propellant weight flow rate) gives the correct specific impulse of 217.5s.

    What is equivalent velocity? ›

    We define a new velocity called the equivalent velocity Veq to be the velocity on the right hand side of the above equation: Veq = Ve + (pe - p0) * Ae / mdot. Then the rocket thrust equation becomes: F = mdot * Veq. The total impulse (I) of a rocket is defined as the average thrust times the total time of firing.

    Which rocket has the highest specific impulse? ›

    The highest specific impulse chemistry ever test-fired in a rocket engine was lithium and fluorine, with hydrogen added to improve the exhaust thermodynamics (all propellants had to be kept in their own tanks, making this a tripropellant).

    What is the relationship between thrust and specific impulse? ›

    Thrust and specific impulse are related by the design and propellants of the engine in question, but this relationship is tenuous. For example, LH2/LO2 bipropellant produces higher Isp but lower thrust than RP-1/LO2 due to the exhaust gases having a lower density and higher velocity (H2O vs CO2 and H2O).

    What is the total impulse of a model rocket? ›

    The total impulse is the integral of the thrust over burn time. is the total impulse in newton seconds. Class A is from 1.26 newton-seconds (conversion factor 4.448 N per lb. force) to 2.5 N·s, and each class is then double the total impulse of the preceding class, with Class B being 2.51 to 5.00 N·s.

    How do you find the impulse of a projectile? ›

    You can also enter the values of mass and velocity change of an object to calculate the impulse from the equation J = mΔv . If you know the force acting on the object, enter the values of force and time change instead. Our impulse and momentum calculator will use the J = Ft formula.

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