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Mass Flow Rate Times Velocity

Force Formula (Rocket Propulsion):

\[ F = W \times V \]

lb/s
ft/s

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1. What is Mass Flow Rate Times Velocity?

Definition: This calculator computes the force generated by a propulsion system based on mass flow rate and exhaust velocity.

Purpose: It helps aerospace engineers and rocket enthusiasts determine the thrust force in pounds (lb) from mass flow rate and velocity.

2. How Does the Calculator Work?

The calculator uses the formula:

\[ F = W \times V \]

Where:

Explanation: The mass flow rate multiplied by velocity gives the thrust force according to basic rocket propulsion principles.

3. Importance of Thrust Calculation

Details: Accurate thrust calculation is essential for rocket design, performance prediction, and ensuring proper acceleration.

4. Using the Calculator

Tips: Enter the mass flow rate in pounds per second (lb/s) and velocity in feet per second (ft/s). All values must be > 0.

5. Frequently Asked Questions (FAQ)

Q1: What units should I use for this calculation?
A: This calculator uses pounds for force (lb), pounds per second for mass flow (lb/s), and feet per second for velocity (ft/s).

Q2: How does this relate to rocket thrust?
A: This is the basic thrust equation where the force equals the mass flow rate times the exhaust velocity relative to the rocket.

Q3: What's a typical mass flow rate for rockets?
A: Large rockets might have mass flow rates of thousands of lb/s, while small model rockets might be fractions of a lb/s.

Q4: Does this account for atmospheric pressure?
A: No, this is the basic equation. Actual thrust would consider nozzle expansion and ambient pressure.

Q5: How do I find mass flow rate in practice?
A: It can be calculated from propellant consumption rate or measured with flow meters in test setups.

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