Reaction engine
engine that produces thrust by expelling reaction mass

A reaction engine is an engine or motor that produces thrust by expelling reaction mass (reaction propulsion), in accordance with Newton's third law of motion. This law of motion is commonly paraphrased as: "For every action force there is an equal, but opposite, reaction force."
Examples include jet engines, rocket engines, pump-jets, and more uncommon variations such as Hall effect thrusters, ion drives, mass drivers, and nuclear pulse propulsion.
Discovery
The discovery of the reaction engine has been attributed to the Romanian inventor Alexandru Ciurcu and to the French journalist Just Buisson.
Energy use
Propulsive efficiency
For all reaction engines that carry on-board propellant (such as rocket engines and electric propulsion drives) some energy must go into accelerating the reaction mass. Every engine wastes some energy, but even assuming 100% efficiency, the engine needs energy amounting to
1
2
M
V
e
2
{\displaystyle {\begin{matrix}{\frac {1}{2}}\end{matrix}}MV_{e}^{2}}
(where M is the mass of propellent expended and
V
e
{\displaystyle V_{e}}
is the exhaust velocity), which is simply the energy to accelerate the exhaust.
Comparing the rocket equation (which shows how much energy ends up in the final vehicle) and the above equation (which shows the total energy required) shows that even with 100% engine efficiency, certainly not all energy supplied ends up in the vehicle – some of it, indeed usually most of it, ends up as kinetic energy of the exhaust.
If the specific impulse (
I
s
p
{\displaystyle I_{sp}}
) is fixed, for a mission delta-v, there is a particular
I
s
p
{\displaystyle I_{sp}}
that minimises the overall energy used by the rocket. This comes to an exhaust velocity of about two-thirds of the mission delta-v (see the energy computed from the rocket equation). Drives with a specific impulse that is both high and fixed such as Ion thrusters have exhaust velocities that can be enormously higher than this ideal, and thus end up powersource limited and give very low thrust. Where the vehicle performance is power limited, e.g.
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Vocabulary and entity names are the principal evidence signals here, because they determine the precision of every later search. The source revision retrieved here is dated Mar 24, 2026. The linked authority identifier is Q1922879. The Library of Congress control number is sh98000239. 1 of 1 selected statements include explicit references; 1 carry qualifiers and 0 use preferred rank.
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