i wanted a design of a turbojet engine that produces 15 to 20 lbf of thrust




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ABSTRACT
An automotive propulsion concept is presented which
utilizes liquid nitrogen as the working fluid for an open
Rankine cycle. Ambient heat exchangers are used to power
an engine that is configured to maximize heat transfer during
the expansion stroke. If sufficient heat input during the
expansion process can be realized then this cryogenic
propulsive system would provide greater automotive ranges
and lower operating costs than those of electric vehicles
currently being considered for mass production.
The
feasibility of meeti ....etc

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seminar report on jet propulsion............ ....etc

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ABSTRACT

The Magneto Hydro Dynamic (MHD) propulsion thruster is designed to use magneto hydrodynamic force generated by sending electric current through a magnetic field created in sea water by superconducting magnets. The principle of MHD propulsion is to apply the Fleming's left hand rule of electromagnetics to sea water directly .In this propulsion system magnetic field is created in sea water by magnets fixed on a hul1. When electric current is sent to sea water at right angles to the magnetic field, and electromagnetic force (Lorentz f ....etc

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Space travel has become a routine in the present world. Space is even a permanent settlement to some astronauts onboard the international Space Station. However, when you think of the size of our solar system, not to mention the universe, we have just taken baby steps into space. Conventional rocket propulsion is based on chemical propulsion systems. Now different methods have been evolved. This seminar will give an overview of some of the advanced propulsion methods like SOLAR THERMAL ROCKET PROPULSION, ELECTROSTATIC ION PROPULSION DRIVES, HAL ....etc

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INTRODUCTION
Spacecraft propulsion is used to change the velocity of spacecraft and artificial satellites. There are many different methods. Each method has drawbacks and advantages, and spacecraft propulsion is an active area of research. Most spacecraft today are propelled by heating the reaction mass and allowing it to flow out the back of the vehicle.For propulsion the required product is the velocity of the exhaust products of the reaction. All current spacecraft use chemical rocket for launch.
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TURBOJET ENGINES

A seminar report is submitted
in partial fulfillment of the requirements
for the final year (8th semester) award of the Degree
of Bachelor of Engineering in
Mechanical Engineering
BY
GAJANAN C AVANTKAR
Under the Guidance of
Prof. M.S.PATIL

DEPARTMENT OF MECHANICAL ENGINEERING
K.L.S SOCIETY’S
GOGTE INSTITUTE OF TECHNOLOGY
BELGAUM-590008


ABSTRACT:
In today’s world it is possible to travel to any part of the world within short span of time
using ai ....etc

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SEMINAR REPORT ON
AIRCRAFT PROPULSION SYSTEM


PRESENTED BY:-
PREETI DWIVEDI
COURSE: B.Tech
COURSE: Mechanical Engineering 3rd year
ROLL No.: 0716540040


GUIDED BY:-

Mr. UC JHA


abstract

Aircrafts come in many different shapes and sizes depending on the mission of the aircraft, but all modern airplanes have certain components in common. These are the fuselage, wing, ta ....etc

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Space travel has become a routine in the present world. Space is even a permanent settlement to some astronauts onboard the international Space Station. However, when you think of the size of our solar system, not to mention the universe, we have just taken baby steps into space. Conventional rocket propulsion is based on chemical propulsion systems. Now different methods have been evolved. This seminar will give an overview of some of the advanced propulsion methods like SOLAR THERMAL ROCKET PROPULSION, ELECTROSTATIC ION PROPULSION DRIVES, HAL ....etc

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Propulsion subsystems in a spacecraft aid in preserving the three-axis stability and the control spin. In addition to it, they also help in carrying out manoeuvres and to bring about slight alterations in trajectory. The superior ones called Ëœenginesâ„¢ can infact, generate an acceleration of large torques in volume to sustain the stability of a solid rocket motor during burning phase. The delta-V for simple tasks like the interplanetary trajectory correction manoeuvres, orbit trim manoeuvres, reaction wheel de-saturation manoeuvres and ....etc

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