Total Impulse Solution

STEP 0: Pre-Calculation Summary
Formula Used
Total impulse = int(Thrust,x,Initial time,Final time)
Tt = int(F,x,t i,tf)
This formula uses 1 Functions, 4 Variables
Functions Used
int - The definite integral can be used to calculate net signed area, which is the area above the x -axis minus the area below the x -axis., int(expr, arg, from, to)
Variables Used
Total impulse - (Measured in Second) - Total impulse is the product of the average thrust and the total time of firing for a rocket.
Thrust - (Measured in Newton) - Thrust is the force produced by the expulsion of high-speed exhaust gases from a rocket engine.
Initial time - (Measured in Second) - Initial time is start time when the force applied.
Final time - (Measured in Second) - Final time is the end time when the force is applied.
STEP 1: Convert Input(s) to Base Unit
Thrust: 5825 Newton --> 5825 Newton No Conversion Required
Initial time: 20 Second --> 20 Second No Conversion Required
Final time: 30 Second --> 30 Second No Conversion Required
STEP 2: Evaluate Formula
Substituting Input Values in Formula
Tt = int(F,x,t i,tf) --> int(5825,x,20,30)
Evaluating ... ...
Tt = 58250
STEP 3: Convert Result to Output's Unit
58250 Second --> No Conversion Required
FINAL ANSWER
58250 Second <-- Total impulse
(Calculation completed in 00.004 seconds)

Credits

Creator Image
Created by LOKESH
Sri Ramakrishna Engineering College (SREC), COIMBATORE
LOKESH has created this Calculator and 25+ more calculators!
Verifier Image
Verified by Harsh Raj
Indian Institute of Technology, Kharagpur (IIT KGP), West Bengal
Harsh Raj has verified this Calculator and 100+ more calculators!

Thrust and Power Generation Calculators

Power required to produce Exhaust Jet Velocity
​ LaTeX ​ Go Power Required = 1/2*Mass Flow Rate*Exit Velocity^2
Thrust given Exhaust Velocity and Mass Flow Rate
​ LaTeX ​ Go Thrust = Mass Flow Rate*Exit Velocity
Thrust given Mass and Acceleration of Rocket
​ LaTeX ​ Go Thrust = Mass of Rocket*Acceleration
Acceleration of Rocket
​ LaTeX ​ Go Acceleration = Thrust/Mass of Rocket

Total Impulse Formula

​LaTeX ​Go
Total impulse = int(Thrust,x,Initial time,Final time)
Tt = int(F,x,t i,tf)

what is total impulse?

Total impulse measures the amount of momentum imparted to a rocket by the motor. It, along with other factors like rocket mass and air drag, determines how high the motor can go.

How to Calculate Total Impulse?

Total Impulse calculator uses Total impulse = int(Thrust,x,Initial time,Final time) to calculate the Total impulse, Total Impulse formula is defined as a measure of the total momentum change produced by a rocket engine during its operation. It quantifies the effectiveness of the propulsion system in generating thrust over a specific time interval. Total impulse is denoted by Tt symbol.

How to calculate Total Impulse using this online calculator? To use this online calculator for Total Impulse, enter Thrust (F), Initial time (t i) & Final time (tf) and hit the calculate button. Here is how the Total Impulse calculation can be explained with given input values -> 58250 = int(5825,x,20,30).

FAQ

What is Total Impulse?
Total Impulse formula is defined as a measure of the total momentum change produced by a rocket engine during its operation. It quantifies the effectiveness of the propulsion system in generating thrust over a specific time interval and is represented as Tt = int(F,x,t i,tf) or Total impulse = int(Thrust,x,Initial time,Final time). Thrust is the force produced by the expulsion of high-speed exhaust gases from a rocket engine, Initial time is start time when the force applied & Final time is the end time when the force is applied.
How to calculate Total Impulse?
Total Impulse formula is defined as a measure of the total momentum change produced by a rocket engine during its operation. It quantifies the effectiveness of the propulsion system in generating thrust over a specific time interval is calculated using Total impulse = int(Thrust,x,Initial time,Final time). To calculate Total Impulse, you need Thrust (F), Initial time (t i) & Final time (tf). With our tool, you need to enter the respective value for Thrust, Initial time & Final time and hit the calculate button. You can also select the units (if any) for Input(s) and the Output as well.
Let Others Know
Facebook
Twitter
Reddit
LinkedIn
Email
WhatsApp
Copied!