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منابع و اعتبارات:

7. VC توربو

6. چرخه دایره

5. کوازیتتورین

4. Thruster X3

3. Skyactiv-X

2. Achates 2.7L

1. پیستون مایع

موسیقی:
"موسیقی محیطی" توسط MasterMusic

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28 پاسخ به “7 قوی ترین موتورهای جدید”

  1. Correction: Rocket engines and other space propulsion systems do not have a "maximum velocity" they can reach, rather they have a maximum efficiency they can achieve. in theory, for a given payload of weight Mp, any type of thruster (chemical, ion, or otherwise) can reach any velocity, it just takes a different mass of fuel, Mf, to get there for engines of varying efficiency. The efficiency, Isp, is measured is meters per second, however its not actually referring to a literal velocity, it's just how the units work out (sometimes its referred to as effective exhaust velocity, but this is just a name, and a confusing one at that). What Isp really represents is the amount of force generated for each kg/s of fuel flow. On any engine, if you increase fuel flow, you increase thrust. But the better the Isp, the more thrust you get for that increase. Now we have everything we need to find out how fast we can go if we know Mp, Mf, and Isp. To find the change in velocity, delta_V, capable, we use the Tsiolkovsky rocket equation, which states:
    delta_V = Isp * ln(Mt/Mp)
    where the total starting mass is Mt = Mp + Mf
    For chemical rockets, the theoretical maximum Isp is around 5,000 m/s while the highest recorded Isp of any ion engine (as far as I am aware) was 189,333 m/s from the DS4G thruster developed by the ESA.

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  3. ok.. put a piston that ratchets a crankshaft ??? omfg the noise would be insane at 100 rpm let alone 2000 where the whole thing rips itself apart trying to move the vehicle or the locking lug on the axle would just fail..

    remember kids… follow the kiss principle or end up with a 50 billion part thing with 40 million more parts that can fail.
    KISS = Keep It Simple Stupid for anyone who never heard of it.

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