Orbital rockets use liquid propellants, often liquid hydrogen + oxygen, to get their large mass off the ground. Burning liquid oxygen produces a tremendous amount of thrust. If the total mass of a rocket, payload, and fuel is kg, what is the necessary thrust (in Newtons) to start the rocket moving from its launch platform?
Details : the acceleration of gravity is on the platform.
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From Newton's second law, we know that F = ma. Here, we are told the total mass of the rocket, payload, and fuel. Multiplying this value by the acceleration of gravity gives the total force (in Newtons) created by this combination of rocket mass and acceleration. This tells us the force created is -19,600,000 N, directed downward towards Earth. Therefore, the rocket needs to create a thrust that has a magnitude equal to or greater than this force, but with an opposite direction (therefore removing the negative sign) to start moving from its launch platform