specific thrust of a RAMJET engine Calculator

The performance of a ramjet engine is typically characterized by key parameters that assess its efficiency and effectiveness in generating thrust. The performance of a ramjet engine can be evaluated using various metrics, including specific thrust, thermal efficiency, and overall thrust.

The specific thrust (TS) is a measure of how much thrust is generated per unit of air mass flow rate. It’s an essential parameter for evaluating the engine’s performance.

Formula for specific thrust (TS):

 

Where:

  • TS is the specific thrust (in Newtons per kilogram per second, N/(kg/s)).
  • T is the thrust generated by the engine (in Newtons, N).
  • ṁ is the air mass flow rate (in kilograms per second, kg/s).

 

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