Calculating Launch Speed: What You Need to Know

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The discussion focuses on calculating the launch speed of a projectile that rises vertically to an altitude equal to one Earth radius. The formula proposed for this calculation is v_{orbit} = √(Gm/r), where G is the universal gravitational constant, m is the mass of the Earth, and r is the radius of the Earth. Participants clarify the components of the formula and its application to orbital mechanics. The conversation emphasizes understanding gravitational forces in relation to launch speed. Accurate calculations are essential for achieving desired altitudes in projectile motion.
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Does anyone know the formula to find launch speed?
 
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Launch in order to do accomplish what?
 
im sorry i think i got it.

its of a projectile that rises vertically above the Earth to an altitude equal to one Earth radius

is it:
square root of: (Universal gravitational constant of earth) x (mass of earth) all divided by Radius of earth?
 
<br /> v_{orbit}=\sqrt{\frac{Gm}{r}}<br />

Where G is universal gravitational constant, m is mass of orbiting body, and r is radius between bodies.
 
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