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AspireSpace
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The British Amateur Space / Rocket Programme |
THE BENEFITS OF HYBRID ROCKET MOTORS |
Hybrid motors
combine good features of both Solid and Liquid Fuelled rockets. They
are controllable, semi storable, cheap and simple. They are based
on the principle of a solid propellant and a liquid oxidiser, and have a
number of features which make them ideal for use in a rocket such as
ASPIRE II, namely:
- Cheapness - Neither the oxidisers (Liquid Oxygen, Hydrogen
Peroxide or Nitrogen Dioxide) or most polymers are particularly
expensive, thus fuel costs are kept to a minimum. The flow lines are also
considerably cheaper than those in a liquid fuelled rocket due to the
simpler arrangement required (since you only have one liquid in the
system, not two).
- Simplicity - Although more complex than a solid rocket motor, a hybrid
motor is considerably simpler to implement than a liquid fuelled engine,
since there is only one set of plumbing required.
- Safety - A hybrid rocket motor offers very safe usage characteristics
over both a solid rocket motor and a liquid fuelled rocket engine.
Combination of the two components, fuel and oxidiser will not cause an
explosion, as can be the case with a liquid fuelled rocket engine, and the hybrid can be turned off at any stage of the flight or on launch. This is
most certainly not possible with a solid rocket motor.
- Environmentally Friendliness - The hybrid motors under
development by AspireSpace burn their propellant at extremely high
temperatures. The result of this is that the only major byproducts in the
rocket's exhaust are Water (in the form of steam), Carbon Monoxide
and Carbon Dioxide (similar to a car exhaust).
Hybrid Motors in general, use non toxic propellants and have fairly benign exhaust products, which
are cleaner than those of solid fuelled rockets, and similar to those
of most liquid fuelled engines. The
exception to this is when maximum performance is required from a
hybrid rocket motor, and every
last drop of propellant is squeezed out of the motor, in
which case the exhaust is less environmentally friendly.
Copyright AspireSpace Rocket Programme, 1997