Kaxa2000
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Assuming a vacuum above the Earth's surface
The discussion revolves around calculating the escape velocity from Earth, focusing on gravitational forces and energy conservation principles.
The discussion is active, with participants questioning the methods and assumptions presented. Some guidance on using energy conservation has been offered, but there is no explicit consensus on the approach to take.
Assumptions include the presence of a vacuum above Earth's surface, and there is a focus on the theoretical aspects of escape velocity calculations without considering practical applications.
The simplest thing to do is to use "conservation of energy". The gravitational force on the rocket is GMm/r2 where G is the universal gravitation constant, M is the mass of the earth, m is the mass of the spaceship and r is the distance from the center of the earth. The work necessary to "escape from earth" is the integral of that, with respect to r, from the surface of the Earth to an infinite distance away. Assuming that you start with initial speed v and apply no more force (not what a spaceship does but the standard way of computing "escape velocity", you must have that much kinetic energy to exchange for potential energy. Set that integral equal to (1/2)mv2 and solve for v. Notice that the mass of the space ship, m, appears on both sides of the equation and can be cancelled.Kaxa2000 said:Assuming a vacuum above the Earth's surface