Aerospace Engineering Lectures - Circular and Escape Velocity, Aerospace Engineering Lecture 61

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circular velocity parabolic velocity escape velocity orbital mechanics space mechanics spacecraft lunar mission moon mission mars mission rocket science physics astronautics

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The circular velocity and escape velocity of a spacecraft are obtained by first getting the equation for eccentricity of the orbit equation. The circular velocity is needed to stay in a circular orbit around the earth and is used for satellites. The escape or parabolic velocity needs to b exceeded for lunar or interplanetary space missions. #aerospaceengineering #spacecraft #gateaerospaceengineering

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