Date: Wed Aug 29 17:21:07 2001
Posted By: David Ellis, Researcher, NASA Lewis Research Center
Area of science: Physics
ID: 996238855.Ph
Message:
How jet and rocket engines work
Jet engines and rocket engines both work using Sir Isaac Newton's Third
Law. For every action there is an equal and opposite reaction. In this
case, a volume of gas is heated and accelerated out the nozzle of an
engine. The gas stream accelerates the craft in the opposite direction.
This produces the thrust to drive the aircraft forward or a space shuttle
into orbit.
The fundamental difference between jet engines and rocket engines is
jet engines use atmospheric oxygen to burn the fuel while rocket engines
carry an oxidizer, typically liquid oxygen.
Would a jet engine work in space?
As you may have guessed from the last paragraph, a jet engine, if oxygen
was supplied to it, would work and produce thrust in space. It would
become a type of rocket engine, though. The currently used method of
burning a fuel in a chamber and using a large volume of superheated gas to
provide thrust is more efficient for space travel, though.
Different types of jet engines
- Ramjet - In a ramjet, air is compressed by the body of the plane and
the inlets as it flows over the plane. Fuel is added and ignited. Hot
gasses expelled from the nozzle provide propulsion. The scramjet uses
supersonic combustion. Sc/ramjets require another propulsion system to
accelerate them to the point where air can be sufficiently compressed.
They are, in principle, the simplest of the jet engines and closest to a
rocket engine. They require no moving parts. An example of a ramjet was
the BOMARC
missile.
- Turbojet - In a turbojet, the compressor at the front of the engine is
driven by a turbine section located in the middle of the engine. Fuel is
added to the compressed air and burned in the combustor section. The hot,
rapidly expanding gasses power the turbine and provide thrust when they
exit at the back of the engine through the nozzle.
- Turboprop - Turboprop is short for turbo-propellor. The design is
almost identical to a turbojet except the compressor section is much
larger. Most of the air is directed out the nozzle rather than into the
engine. This air provides thrust in a manner similar to a propellor on a
WWI era plane but at much higher efficiency.
Related Web sites
Some suggested reading
- Constant, Edward W., II, The Origins of the Turbojet Revolution
(1981)
- Cumpsty, Nicholas, Jet Propulsion: A Simple Guide to the Aerodynamic
and Thermodynamic Design of Jet Engines (1997)
- Gunston, Bill, The Development of Jet and Turbo Aero Engines
(1995)
- Hosny, A. N., Propulsion Systems, rev. ed. (1974)
- Rolls-Royce, Ltd., The Jet Engine, 4th ed. (1986)
- G.P. Sutton, Rocket Propulsion Elements, Fifth Ed., (1986)
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