Formula & Calculator
Thrust Specific Fuel Consumption (TSFC)
Fuel mass flow rate consumed per unit of thrust produced, a key measure of jet engine fuel efficiency.
Variables
| Symbol | Quantity | Unit |
|---|---|---|
| TSFC | Thrust specific fuel consumption | kg/(N*s) |
| mdot_f | Fuel mass flow rate | kg/s |
| T | Thrust | N |
What it means
TSFC is a key engine performance parameter, indicating how much fuel is consumed per unit thrust. It is typically expressed in kg/(N·s) or lb/(lbf·h). Lower TSFC means better fuel economy. TSFC varies with altitude, speed, and throttle setting. It is used in the Breguet range equation and in mission analysis. Understanding TSFC is essential for comparing engines and for evaluating propulsion system efficiency.
Worked example
TSFC – Two Examples
Real‑World| Parameter | Value |
|---|---|
| ṁ_f | 0.36 kg/s |
| T | 20,000 N |
| Parameter | Value |
|---|---|
| ṁ_f | 0.5 |
| T | 25,000 |
Common mistakes
- Thrust specific fuel consumption: TSFC = ṁ_f / T.
- Units: kg/(N·s) or 1/s (since N = kg·m/s², so kg/(N·s) = kg/(kg·m/s²·s) = s/m? Actually, TSFC is typically given in kg/(N·h) or lb/(lbf·h). In SI, it’s kg/(N·s).
- Lower TSFC means better fuel efficiency.
- Typical values: 0.5‑0.9 lb/(lbf·h) for turbofans.
Applications
Thrust specific fuel consumption (TSFC), TSFC = ṁ_f / T, is the fuel flow rate per unit thrust, a measure of engine efficiency. Lower TSFC means less fuel for a given thrust, leading to better range and endurance. Engineers use TSFC to compare engines, to design propulsion systems, and to predict mission performance. It is a key parameter in the Breguet equations. By reducing TSFC through advanced cycles and materials, aerospace engineers can improve aircraft efficiency and reduce emissions.
- Engine selection and performance comparison
- Mission performance prediction (range, endurance)
- Propulsion system design and optimisation
- Technology roadmapping for next‑generation engines
- Economic and environmental analyses