Enter the total thrust (N), the chamber pressure (Pa), and the throat area (m^2) into the Thrust Coefficient Calculator. The calculator will evaluate the Thrust Coefficient.

## Thrust Coefficient Formula

The following formula is used to calculate the Thrust Coefficient.

TC = F / (Pc * At)

Variables:

- TC is the Thrust Coefficient ( )
- F is the total thrust (N)
- Pc is the chamber pressure (Pa)
- At is the throat area (m^2)

To calculate a thrust coefficient, divide the total thrust by the product of the chamber pressure and throat area.

## How to Calculate Thrust Coefficient?

The following steps outline how to calculate the Thrust Coefficient.

- First, determine the total thrust (N).
- Next, determine the chamber pressure (Pa).
- Next, determine the throat area (m^2).
- Next, gather the formula from above = TC = F / (Pc * At).
- Finally, calculate the Thrust Coefficient.
- After inserting the variables and calculating the result, check your answer with the calculator above.

**Example Problem:**

Use the following variables as an example problem to test your knowledge.

total thrust (N) = 300

chamber pressure (Pa) = 10

throat area (m^2) = 20

TC = F / (Pc * At) =** ** ?