Rocket engines
At their simplest, liquid-propellant
rocket engines are just high-pressure blast chambers with liquid fuel
and liquid oxygen pumped in at one end, and hot exhaust gases escaping
from a nozzle at the other end.
The fuel and oxygen are pumped in at
very high pressure, the fuel burns in the confined chamber and creates
exhaust gases which are forced at high pressure and speed towards
the exhaust nozzle. The cone-shaped nozzle accelerates the gases even
further, so that they blast away from the rear of the engine at anything
up 16,000 kilometres per hour.
Solid fuel rocket engines are simply
cylinders packed with a propellant. The important thing is that the
propellant burns rapidly, but does not explode.
The propellant must have a hollow tube
drilled down its length. When the rocket is ignited, the fuel burns
along the entire length of the tube, and the exhaust gases are forced
out of the nozzle at the base of the rocket. The tube gets wider and
wider until all the fuel has burned away