Please help me with this question. I got a m = m0 * e^(-gt/Vex) for part a, but not sure about it. Thanks for the help.
Please help me with this question. I got a m = m0 * e^(-gt/Vex) for part...
3. A SpaceX StarshipTM single-stage rocket is launched vertically from the moons surface. It burns k kg of fuel per second, so its mass as a function of time is m = mo - kt. Assume constant acceleration of gravity g and a constant exhaust speed of vex (a) By integrating with respect to time, calculate the rockets velocity versus time (while it still has fuel). (b) Integrate again to show that the altitude versus time is given by (e)...