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Means to Create A Jet

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Means to Create A Jet

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    1. Means to Create A Jet P M V Subbarao Professor Mechanical Engineering Department

    3. Jet Characteristics of Practical Propulsion Systems

    4. Nozzle : Steady State Steady Flow

    6. How to Create A Jet?

    7. How and What to do?

    9. Engines to Create a Jet ???

    10. UFO Logistics Is It Really Possible That The Ancient Indians Had The Capacity To Deploy Devastating Nuclear Weapons Against Their Enemies? Moreover, Is It Really Possible, As Many Ufologists Claim, That Awesomely Powerful Nuclear Weapons Were Actually Given To The Ancient Indian Warriors By Extra-tererstrials, Highly Advanced Spacemen From Other Planets? Well, Passages From Ancient Indian National Epics Certainly Appear To Be Evidence Of Such Astonishing Claims…. Http://Www.Ufoevidence.Org/Documents/Doc1937.Htm

    11. “The heavens cried out, the earth bellowed an answer, lightening flashed forth, fire flamed upwards, it rained down death. The brightness vanished, the fire was extinguished. Everyone who was struck by the lightening was turned to ashes”. And again from the same source: “It was a ghastly sight to see. The corpses of the fallen were so mutilated they no longer looked like human beings. Never before have we seen such an awful weapon, and never before have we heard of such a weapon”.

    12. The Ancient Technique : Ramjets Only three operating components: intake (diffuser); burner (combustion chamber); nozzle.

    13. 13 Ramjets - Basic Operating Features

    14. 14 Ramjets (Front Intake) for GW

    15. Introduction to Rockets

    16. Solid Propellant Rocket - Basic Operating Features Four basic components: motor case, nozzle, solid propellant charge, igniter. Propellant charge comprises combined fuel & oxidizer. Gaseous combustion products fill void at high pressure (70 bar typically) and sustains combustion. Hot gases vent through convergent-divergent nozzle to provide high-speed (supersonic) propulsion jet. Gases generated and escape at fixed rate for steady operation by maintaining constant burning surface area.

    17. Solid Propellant Rocket for GW

    18. Solid Rocket Features High propellant density (volume-limited designs). Long-lasting chemical stability. Readily available, tried and trusted, proven in service. No field servicing equipment & straightforward handling. Cheap, reliable, easy firing and simple electrical circuits. But Lower specific impulses (compared with liquid rockets). Difficult to vary thrust on demand. Smokey exhausts (especially with composite propellants). Performance affected by ambient temperature.

    19. Liquid Propellant Rocket - Basic Operating Features Fuel and oxidant tanked separately and delivered to combustion chamber at specific rates and pressures. Propellant flowrates (and hence thrust) variable upon demand. Disadvantages compared with solid propellant rockets: increased complication; Storage problems (usually LOX & LH2 which must be maintained at very low temperatures); more costly; reduced reliability.

    20. Liquid Propellant Rocket - Space

    21. Space Transportation System (STS)

    22. Closure Ramjet Advantages: -Low Weight -High Thrust to Weight Ratio. -No moving parts keep initial and maintenance costs down. -Large Thrust to Unit Frontal Area. -Provides best specific fuel consumption of all air breathing engines at supersonic speeds. Ramjet Disadvantages: -Does not work well at off design Mach numbers without a variable geometry diffuser and supersonic spike. -By the nature of air compression, does not provide static thrust. -Fuel consumption at subsonic speeds is very high compared to other air breathing engines.

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