Thrust power specific fuel consumption Solution

STEP 0: Pre-Calculation Summary
Formula Used
Thrust Power Specific Fuel Consumption = Fuel Flow Rate/Thrust Power
TPSFC = mf/TP
This formula uses 3 Variables
Variables Used
Thrust Power Specific Fuel Consumption - (Measured in Kilogram per Second per Watt) - Thrust Power Specific Fuel Consumption is the measures of the overall thermal efficiency of an engine for a given air speed and jet speed.
Fuel Flow Rate - (Measured in Kilogram per Second) - Fuel Flow Rate refers to the rate at which fuel is supplied or consumed within a system over a specified period.
Thrust Power - (Measured in Watt) - Thrust Power refers to the power generated by a propulsion system to produce thrust and propel an object forward.
STEP 1: Convert Input(s) to Base Unit
Fuel Flow Rate: 0.0315 Kilogram per Second --> 0.0315 Kilogram per Second No Conversion Required
Thrust Power: 54 Kilowatt --> 54000 Watt (Check conversion ​here)
STEP 2: Evaluate Formula
Substituting Input Values in Formula
TPSFC = mf/TP --> 0.0315/54000
Evaluating ... ...
TPSFC = 5.83333333333333E-07
STEP 3: Convert Result to Output's Unit
5.83333333333333E-07 Kilogram per Second per Watt -->2.1 Kilogram per Hour per Kilowatt (Check conversion ​here)
FINAL ANSWER
2.1 Kilogram per Hour per Kilowatt <-- Thrust Power Specific Fuel Consumption
(Calculation completed in 00.004 seconds)

Credits

Creator Image
Created by Chilvera Bhanu Teja
Institute of Aeronautical Engineering (IARE), Hyderabad
Chilvera Bhanu Teja has created this Calculator and 300+ more calculators!
Verifier Image
Verified by Sagar S Kulkarni
Dayananda Sagar College of Engineering (DSCE), Bengaluru
Sagar S Kulkarni has verified this Calculator and 200+ more calculators!

Thrust Generation Calculators

Total Thrust given Efficiency and Enthalpy
​ LaTeX ​ Go Total Thrust = Mass Flow Rate*((sqrt(2*Enthalpy Drop in Nozzle*Nozzle Efficiency))-Flight Speed+(sqrt(Turbine Efficiency*Efficiency of Transmission*Enthalpy Drop in Turbine)))
Thrust power
​ LaTeX ​ Go Thrust Power = Mass Flow Rate*Flight Speed*(Exit Velocity-Flight Speed)
Ideal Thrust given Effective Speed Ratio
​ LaTeX ​ Go Ideal Thrust = Mass Flow Rate*Flight Speed*((1/Effective Speed Ratio)-1)
Specific thrust
​ LaTeX ​ Go Specific Thrust = Exit Velocity-Flight Speed

Thrust power specific fuel consumption Formula

​LaTeX ​Go
Thrust Power Specific Fuel Consumption = Fuel Flow Rate/Thrust Power
TPSFC = mf/TP

What is thrust power?

The thrust developed by the engine overcomes the drag on the aircraft and in doing so it develops power, called the thrust power.

How to Calculate Thrust power specific fuel consumption?

Thrust power specific fuel consumption calculator uses Thrust Power Specific Fuel Consumption = Fuel Flow Rate/Thrust Power to calculate the Thrust Power Specific Fuel Consumption, Thrust power specific fuel consumption is a measure of the amount of fuel consumed per unit of thrust power produced by an aircraft or rocket engine, calculated by dividing the fuel flow rate by the thrust power. This metric is essential for evaluating the efficiency and performance of an aircraft or rocket engine. Thrust Power Specific Fuel Consumption is denoted by TPSFC symbol.

How to calculate Thrust power specific fuel consumption using this online calculator? To use this online calculator for Thrust power specific fuel consumption, enter Fuel Flow Rate (mf) & Thrust Power (TP) and hit the calculate button. Here is how the Thrust power specific fuel consumption calculation can be explained with given input values -> 7.6E+6 = 0.0315/54000.

FAQ

What is Thrust power specific fuel consumption?
Thrust power specific fuel consumption is a measure of the amount of fuel consumed per unit of thrust power produced by an aircraft or rocket engine, calculated by dividing the fuel flow rate by the thrust power. This metric is essential for evaluating the efficiency and performance of an aircraft or rocket engine and is represented as TPSFC = mf/TP or Thrust Power Specific Fuel Consumption = Fuel Flow Rate/Thrust Power. Fuel Flow Rate refers to the rate at which fuel is supplied or consumed within a system over a specified period & Thrust Power refers to the power generated by a propulsion system to produce thrust and propel an object forward.
How to calculate Thrust power specific fuel consumption?
Thrust power specific fuel consumption is a measure of the amount of fuel consumed per unit of thrust power produced by an aircraft or rocket engine, calculated by dividing the fuel flow rate by the thrust power. This metric is essential for evaluating the efficiency and performance of an aircraft or rocket engine is calculated using Thrust Power Specific Fuel Consumption = Fuel Flow Rate/Thrust Power. To calculate Thrust power specific fuel consumption, you need Fuel Flow Rate (mf) & Thrust Power (TP). With our tool, you need to enter the respective value for Fuel Flow Rate & Thrust Power and hit the calculate button. You can also select the units (if any) for Input(s) and the Output as well.
Let Others Know
Facebook
Twitter
Reddit
LinkedIn
Email
WhatsApp
Copied!