Rocket Propellant Solid or Liquid
A guide to the concept of Mechanical
Engineering at Arya College
The rocket propellant is the chemical mixture that is burned to
produce thrust in rockets. It consists of a fuel and an oxidizer. Fuel is a
substance that can be in a liquid or solid state, burns when combined with
oxygen producing gases for propulsion. An oxidizer is an agent that releases
oxygen in combination with a fuel.
Rockets
propellants for Mechanical Engineering at B Tech College in Jaipur can be
classified according to their state as:
1.
Solid propellant
2.
Liquid propellant
3.
Hybrid (a mixture of
solid and liquid propellant).
Solid Propellant Rockets
The solid propellant rocket motor mainly consists of a seamless
tube. They are made of steel, closed solidify at one end. The open end holds
the nozzle which may be a single or multi-orifice type.
The solid propellant rockets divide into two main types
according to the amount of surface area exposes to burning. These two types
are:
1.
The restricted burning
rocket is one in which the propellant constrains to burn on only one surface.
The manner in which cigarette burns is similar to the type of burning of a
restricted burning rocket.
2.
The unrestricted
burning rockets mostly free to burn on all surfaces at the same time.
The
restricted burning rocket delivers a small thrust for a relatively long period
for the students of Top Engineering College in
Jaipur who is experimenting different machines while the
unrestricted flaming rocket provides a relatively large thrust for a short
period.
Liquid Propellant Rocket ?????
To read continue
with ARYA COLLEGE
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