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NASA Thrust Equation gets destroyed.
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[quote:Anonymous Coward 76708078:MV8zOTg5OTIyXzcyMjAyODUyXzc3RUY2REQz] [quote:Anonymous Coward 4448622:MV8zOTg5OTIyXzcyMjAyNzc2XzQ5RTg4Qzc1] [quote:Anonymous Coward 76708078:MV8zOTg5OTIyXzcyMTk4Nzg2XzJBNDk2MDAx] [quote:Anonymous Coward 77414673:MV8zOTg5OTIyXzcyMTk4Mzk0X0RBNTU5OEIw] [quote:Anonymous Coward 76708078:MV8zOTg5OTIyXzcyMTk4MDU2XzlBQTgwOEM5] [quote:Hungdaddy69 70390093:MV8zOTg5OTIyXzcyMTk3ODg0Xzk3Nzg1NjQ2] Absolute :bs2:. [/quote] you can't bs math [/quote] Bad interpretations of facts, even using math, can be BS, though. [/quote] It’s not bs. The fluid dynamics equation is used in Many industries. The velocity of gas in the nozzle pipe is equal to the exit velocity. [/quote] ...and it is mass that's being accelerated out of the combustion chamber and out of the rocket engine nozzle. The fuel and oxidizer molecules don't just "go away" at ignition. [/quote] Ummm....That's why it's called mass flow rate. [/quote]
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