Category: Launch

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Launch

Launch Equations

Earth escape velocity using r only MichaelBartmess Use Equation
Earth escape velocity using $μ$ $mu$ MichaelBartmess Use Equation
Earth escape velocity using $R_{E}$ $R_E$ MichaelBartmess Use Equation
$R = (\frac{2 v^{2}}{g}) \sin (θ) \cos (θ)$ $R = ((2v^2)/g) sin(theta) cos(theta)$ KurtHeckman Use Equation

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