A system of pyrotechny : $b Comprehending the theory and practice, with the application of chemistry; designed for exhibition and for war.Cutbush, James
History
A system of pyrotechny : $b Comprehending the theory and practice, with the application of chemistry; designed for exhibition and for war.
Cutbush, James
Fireworks; Military fireworks
Mariotte and Desaguliers have given two distinct theories of the
motion of rockets. The latter ascribes their motion to the momentum
of combustion, and the former to the elastic nature of the gaseous
fluid, generated by the combustion, and the resistance of air. The
observations of Desaguliers are the following: "Conceive the rocket
to have no vent at the choke, and to be set on fire, the consequence
will be, either that the rocket will burst in the weakest place,
or if all the parts be equally strong, and be able to sustain the
impulse of the flame, the rocket would burn out immoveable. Now, as
the force of the flame is equable, suppose its action downwards, or
that upwards, to lift 40 pounds; as these forces are equal, but their
directions contrary, they will destroy each other's action. Imagine
then the rocket opened at the choke; by this means, the action of the
flame downwards is taken away, and there remains a force equal to
forty pounds, acting upwards, to carry up the rocket and stick." This
theory, however ingenious, is not altogether true; for it is asserted
on the contrary, that the action of the flame or gas within the
rocket, when closed, as supposed above, is conceived to arise wholly
from the elastic nature of the gas, and the reaction it experiences
against the ends and sides of the rocket-case; the whole of which
ceases as soon as a free vent is given to the flame; and, therefore,
if a rocket could be fixed in a vacuum, as the flame would, in that
case, experience no resistance, there would be no reaction, and
consequently, no motion would ensue. Some experiments, analogous to
this position, have been made. We may merely add, with respect to
Mariotte's theory, that he attributes the motion of the rocket to
the resistance and reaction of the air, in consequence of which the
propelling force will decrease as the velocity increases, owing to
the partial vacuum left behind the rocket in its flight; so that the
correct solution of the problem necessarily involves the integration
of partial differences of the highest orders.
Public-domain text, read in full here on John Shaqi.
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