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F = q(v x B) kinetic energy = ½ mv2 How much of a rocket must its fuel take up: Propellant mass/delivered mass = [e(Dv/vj) -1] where Dv is change in velocity, and vj is the velocity of the exhaust gas. Delivered mass includes the structure of the rocket itself. Penetration Depth of a Hypervelocity Impact:
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| © 2013 Carolyn Meinel | ||||||||||