Thrust-to-weight ratio Calculator

✖Drag Coefficient is a dimensionless quantity that is used to quantify the drag or resistance of an object in a fluid environment, such as air or water.ⓘ Drag Coefficient [C_D]			+10% -10%
✖The Lift Coefficient is a dimensionless coefficient that relates the lift generated by a lifting body to the fluid density around the body, the fluid velocity and an associated reference area.ⓘ Lift Coefficient [C_L]			+10% -10%

✖Thrust-to-Weight Ratio is a dimensionless ratio of thrust to weight of a rocket, jet engine, propeller engine.ⓘ Thrust-to-weight ratio [TW]

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Thrust-to-weight ratio Solution

STEP 0: Pre-Calculation Summary

Formula Used

Thrust-to-Weight Ratio = Drag Coefficient/Lift Coefficient
TW = C_D/C_L
This formula uses 3 Variables

Variables Used

Thrust-to-Weight Ratio - Thrust-to-Weight Ratio is a dimensionless ratio of thrust to weight of a rocket, jet engine, propeller engine.
Drag Coefficient - Drag Coefficient is a dimensionless quantity that is used to quantify the drag or resistance of an object in a fluid environment, such as air or water.
Lift Coefficient - The Lift Coefficient is a dimensionless coefficient that relates the lift generated by a lifting body to the fluid density around the body, the fluid velocity and an associated reference area.

STEP 1: Convert Input(s) to Base Unit

Drag Coefficient: 0.5 --> No Conversion Required
Lift Coefficient: 1.1 --> No Conversion Required

STEP 2: Evaluate Formula

Substituting Input Values in Formula

TW = C_D/C_L --> 0.5/1.1

Evaluating ... ...

TW = 0.454545454545455

STEP 3: Convert Result to Output's Unit

0.454545454545455 --> No Conversion Required

FINAL ANSWER

0.454545454545455 ≈ 0.454545 <-- Thrust-to-Weight Ratio

(Calculation completed in 00.004 seconds)

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Credits

Created by Vinay Mishra

Indian Institute for Aeronautical Engineering and Information Technology (IIAEIT), Pune

Vinay Mishra has created this Calculator and 300+ more calculators!

Verified by Sanjay Krishna

Amrita School of Engineering (ASE), Vallikavu

Sanjay Krishna has verified this Calculator and 200+ more calculators!

< Thrust and Power Requirements Calculators

Thrust Angle for Unaccelerated Level Flight for given Lift

LaTeX Go Thrust Angle = asin((Weight of Body-Lift Force)/Thrust)

Weight of Aircraft in Level, Unaccelerated Flight

LaTeX Go Weight of Body = Lift Force+(Thrust*sin(Thrust Angle))

Thrust for Level and Unaccelerated Flight

LaTeX Go Thrust = Drag Force/(cos(Thrust Angle))

Thrust Angle for Unaccelerated Level Flight for given Drag

LaTeX Go Thrust Angle = acos(Drag Force/Thrust)

Thrust-to-weight ratio Formula

LaTeX Go

Thrust-to-Weight Ratio = Drag Coefficient/Lift Coefficient
TW = C_D/C_L

What is a good thrust to weight ratio for rockets?

For rockets, a minimum acceptable Thrust to weight(rocket and installed motors) ratio of 5:1 is typically required.

How to Calculate Thrust-to-weight ratio?

Thrust-to-weight ratio calculator uses Thrust-to-Weight Ratio = Drag Coefficient/Lift Coefficient to calculate the Thrust-to-Weight Ratio, Thrust-to-weight ratio is a measure used in aerospace engineering to assess the power-to-weight ratio of a vehicle, typically an aircraft or a rocket, it compares the amount of thrust generated by the propulsion system to the weight of the vehicle. Thrust-to-Weight Ratio is denoted by TW symbol.

How to calculate Thrust-to-weight ratio using this online calculator? To use this online calculator for Thrust-to-weight ratio, enter Drag Coefficient (C_D) & Lift Coefficient (C_L) and hit the calculate button. Here is how the Thrust-to-weight ratio calculation can be explained with given input values -> 0.454545 = 0.5/1.1.

FAQ

What is Thrust-to-weight ratio?

Thrust-to-weight ratio is a measure used in aerospace engineering to assess the power-to-weight ratio of a vehicle, typically an aircraft or a rocket, it compares the amount of thrust generated by the propulsion system to the weight of the vehicle and is represented as TW = C_D/C_L or Thrust-to-Weight Ratio = Drag Coefficient/Lift Coefficient. Drag Coefficient is a dimensionless quantity that is used to quantify the drag or resistance of an object in a fluid environment, such as air or water & The Lift Coefficient is a dimensionless coefficient that relates the lift generated by a lifting body to the fluid density around the body, the fluid velocity and an associated reference area.

How to calculate Thrust-to-weight ratio?

Thrust-to-weight ratio is a measure used in aerospace engineering to assess the power-to-weight ratio of a vehicle, typically an aircraft or a rocket, it compares the amount of thrust generated by the propulsion system to the weight of the vehicle is calculated using Thrust-to-Weight Ratio = Drag Coefficient/Lift Coefficient. To calculate Thrust-to-weight ratio, you need Drag Coefficient (C_D) & Lift Coefficient (C_L). With our tool, you need to enter the respective value for Drag Coefficient & Lift Coefficient and hit the calculate button. You can also select the units (if any) for Input(s) and the Output as well.

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