Recent content by camdickman

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    Acceleration, thrust, and propellant velocity?

    Homework Statement What is the average acceleration until burnout of a spacecraft engine creating 53.2MN of thrust with a propellant velocity of 4.78km/s? The initial mass is 2.12x10^6 kg and final ,*** is 7.04x10^4. Homework Equations 0 = m(subscript_f)v(_f) + m(_r)v(_r) The...
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