Specific impulse
how efficiently a reaction mass engine creates thrust, which is often proportional to effective exhaust gas velocity

Specific impulse (usually abbreviated as Isp) is a physical quantity defined as the ratio of change in momentum (impulse) to the mass used, usually fuel. It typically uses units of metres per second (a SI unit) or feet per second (in imperial units). It is equivalent to thrust (a force, in newtons or pounds) per mass flow rate (in kg/s or lbm/s).
It serves as a measure of how efficiently an engine, such as a rocket or jet engine, generates thrust from propellant. Isp is the effective exhaust velocity used in the Tsiolkovsky rocket equation which calculates how much a vehicle's velocity can be changed with a given quantity of fuel.
Normalized specific impulse is the ratio of specific impulse to Earth's standard acceleration of gravity, g (in m/s2 or ft/s2). It is measured in seconds, and conveniently is the same number in both SI and imperial units. It can be understood as the time that one kilogram of fuel can produce one kilogram-force of thrust, which is equal to the time that one pound-mass of fuel can produce one pound-force of thrust.
Overview
Reaction engines, such as rockets and jet engines propel a vehicle by expelling mass in one direction, which pushes the vehicle in the other direction according to Newton's third law of motion. This expelled mass is called the reaction mass.
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