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Thrust Specific Fuel Consumption (TSFC)

TSFC is the fuel flow rate divided by thrust. It tells you how much fuel a jet engine burns to produce one unit of thrust for one hour. Lower is better. For example, a modern high-bypass turbofan has a TSFC of about 0.5-0.6 kg/(N·h), while an older turbojet might be 0.9-1.0. This number is the single most important measure of jet engine fuel efficiency. It directly affects aircraft range and airline operating costs. It is roughly the inverse of specific impulse.

Propulsion Aircraft Performance Efficiency

Calculate TSFC

Switch between a quick basic calculation and the full advanced propulsion analysis mode.

FUEL PARAMETERS
kg/m³
MJ/kg
ENGINE PARAMETERS
:1
:1
FLIGHT PARAMETERS
M
°C
kPa
MISSION PARAMETERS
hr
kg
kg

Interactive Analysis Graphs

Generated live from your Advanced Mode inputs. Run the analysis above to populate.

TSFC vs Thrust

Sensitivity of TSFC as net thrust varies, fuel flow held constant.

TSFC vs Altitude

Approximate trend as ambient temperature falls with altitude.

TSFC vs Mach Number

Illustrative TSFC trend across the flight Mach range.

Fuel Burn Rate

Fuel burn per hour, per kilometre, and per nautical mile.

Aircraft Range Sensitivity

Estimated range as available fuel weight changes.

Engineering Reference Tables

Typical values used to sanity-check a calculation against real hardware.

Typical TSFC Values by Engine Type
Engine TypeTypical TSFC (lb/lbf·hr)Typical TSFC (kg/N·hr)Notes
Aircraft Examples
AircraftEngineCruise TSFC (lb/lbf·hr)Category
Fuel Properties
FuelDensity (kg/m³)Heating Value (MJ/kg)Energy Content (MJ/L)

How Engineers Use TSFC

Practical applications across the aircraft lifecycle.

Engine Comparison Module

Compare TSFC, fuel burn, and range impact across three engines side by side.

Engine A

Engine B

Engine C

EngineTSFC (kg/N·hr)Fuel Burn (kg/hr)Relative EfficiencyRange Impact

Scenario Simulator

One-click presets that populate Advanced Mode with representative values.

Understanding TSFC

Grounding for students and anyone new to propulsion performance metrics.

Formula Library

The core equations behind this calculator, with short derivations.

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
Scenario: Fuel flow ṁ_f = 0.36 kg/s, thrust T = 20,000 N. Find TSFC.
ParameterValue
ṁ_f0.36 kg/s
T20,000 N
1TSFC = ṁ_f/T = 0.36/20000 = 1.8×10⁻⁵ kg/(N·s)
Result 1.8×10⁻⁵ ✓ Efficient
Scenario: ṁ_f = 0.5, T = 25,000. Find TSFC.
ParameterValue
ṁ_f0.5
T25,000
1TSFC = 0.5/25000 = 2.0×10⁻⁵ kg/(N·s)
Result 2.0×10⁻⁵ ✓ Typical
Key insight: TSFC is fuel consumption per unit thrust – lower is more efficient.

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

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  • Published July 10, 2026
  • Last updated October 4, 2026