FormulaDen.com

Physics Chemistry Math Chemical Engineering Civil Electrical Electronics Electronics and Instrumentation Materials Science Mechanical Production Engineering Financial Health

Thrust given Exhaust Velocity and Mass Flow Rate Formula

GoThrust given Mass and Acceleration of Rocket Formula

GoPhoton Propulsion Thrust Formula

Fx Copy

LaTeX Copy

Thrust is the force produced by the expulsion of high-speed exhaust gases from a rocket engine. Check FAQs

F = m a \cdot C j

F - Thrust?m_a - Mass Flow Rate?C_j - Exit Velocity?

Thrust given Exhaust Velocity and Mass Flow Rate Example

With values

With units

Only example

Here is how the Thrust given Exhaust Velocity and Mass Flow Rate equation looks like with Values.

Here is how the Thrust given Exhaust Velocity and Mass Flow Rate equation looks like with Units.

Here is how the Thrust given Exhaust Velocity and Mass Flow Rate equation looks like.

5825.52 = 23.49 \cdot 248

5825.52N = 23.49kg/s \cdot 248m/s

5825.52 = 23.49 \cdot 248

Tip: Use pencil ( Pencil

) icon above to edit Input Values and Units.

Calculate

Recalculate

Solution

Copy

Reset

You are here -

Home » Category

Physics » Category

Aerospace » Category

Propulsion » fx Thrust given Exhaust Velocity and Mass Flow Rate

Thrust given Exhaust Velocity and Mass Flow Rate Solution

Follow our step by step solution on how to calculate Thrust given Exhaust Velocity and Mass Flow Rate?

FIRST Step Consider the formula

F = m a \cdot C j

Next Step Substitute values of Variables

∴

F = 23.49kg/s \cdot 248m/s

Next Step Prepare to Evaluate

∴

F = 23.49 \cdot 248

LAST Step Evaluate

∴

F = 5825.52N

Thrust given Exhaust Velocity and Mass Flow Rate Formula Elements

Variables

Thrust

Thrust is the force produced by the expulsion of high-speed exhaust gases from a rocket engine.

Symbol: F

Measurement: ForceUnit: N

Note: Value should be greater than 0.

Formulas to find Thrust

Mass Flow Rate

Mass Flow Rate represents the amount of mass passing through a system per unit of time.

Symbol: m_a

Measurement: Mass Flow RateUnit: kg/s

Note: Value should be greater than 0.

Formulas to find Mass Flow Rate

Exit Velocity

Exit Velocity is the speed at which exhaust gases exit the primary nozzle of a propulsion system, such as a rocket or jet engine.

Symbol: C_j

Measurement: SpeedUnit: m/s

Note: Value should be greater than 0.

Formulas to find Exit Velocity

Other Formulas to find Thrust

Go Thrust given Mass and Acceleration of Rocket

F = m \cdot a

Go Photon Propulsion Thrust

F = 1000 \cdot \frac{P e}{[c]}

Other formulas in Thrust and Power Generation category

Go Power required to produce Exhaust Jet Velocity

P = \frac{1}{2} \cdot m a \cdot {C j}^{2}

Go Acceleration of Rocket

a = \frac{F}{m}

Go Power required to produce Exhaust Jet Velocity given Mass of Rocket and Acceleration

P = \frac{m \cdot a \cdot V eff}{2}

Go Exit Velocity given Mach Number and Exit Temperature

C j = M \cdot \sqrt{γ \cdot \frac{[R]}{M molar} \cdot T exit}

How to Evaluate Thrust given Exhaust Velocity and Mass Flow Rate?

Thrust given Exhaust Velocity and Mass Flow Rate evaluator uses Thrust = Mass Flow Rate*Exit Velocity to evaluate the Thrust, Thrust given Exhaust Velocity and Mass Flow Rate formula is defined as a means to quantify the force produced by a rocket engine, based on the velocity of the exhaust gases and the rate at which mass is expelled. Thrust is denoted by F symbol.

How to evaluate Thrust given Exhaust Velocity and Mass Flow Rate using this online evaluator? To use this online evaluator for Thrust given Exhaust Velocity and Mass Flow Rate, enter Mass Flow Rate (m_a) & Exit Velocity (C_j) and hit the calculate button.

FAQs on Thrust given Exhaust Velocity and Mass Flow Rate

What is the formula to find Thrust given Exhaust Velocity and Mass Flow Rate?

The formula of Thrust given Exhaust Velocity and Mass Flow Rate is expressed as Thrust = Mass Flow Rate*Exit Velocity. Here is an example- 5825.52 = 23.49*248.

How to calculate Thrust given Exhaust Velocity and Mass Flow Rate?

With Mass Flow Rate (m_a) & Exit Velocity (C_j) we can find Thrust given Exhaust Velocity and Mass Flow Rate using the formula - Thrust = Mass Flow Rate*Exit Velocity.

What are the other ways to Calculate Thrust?

Here are the different ways to Calculate Thrust-

Thrust=Mass of Rocket*Acceleration
Thrust=1000*Power in Jet/[c]

Can the Thrust given Exhaust Velocity and Mass Flow Rate be negative?

No, the Thrust given Exhaust Velocity and Mass Flow Rate, measured in Force cannot be negative.

Which unit is used to measure Thrust given Exhaust Velocity and Mass Flow Rate?

Thrust given Exhaust Velocity and Mass Flow Rate is usually measured using the Newton[N] for Force. Exanewton[N], Meganewton[N], Kilonewton[N] are the few other units in which Thrust given Exhaust Velocity and Mass Flow Rate can be measured.

Let Others Know

✖

Facebook

Twitter

Copied!

: Value
: Unit

Thrust given Exhaust Velocity and Mass Flow Rate Formula

​GoThrust given Mass and Acceleration of Rocket Formula

​GoPhoton Propulsion Thrust Formula

Thrust given Exhaust Velocity and Mass Flow Rate Example

Thrust given Exhaust Velocity and Mass Flow Rate Solution

Thrust given Exhaust Velocity and Mass Flow Rate Formula Elements

Other Formulas to find Thrust

Other formulas in Thrust and Power Generation category

How to Evaluate Thrust given Exhaust Velocity and Mass Flow Rate?

FAQs on Thrust given Exhaust Velocity and Mass Flow Rate

Variable Name

GoThrust given Mass and Acceleration of Rocket Formula

GoPhoton Propulsion Thrust Formula