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Fuel is ejected from a rocket of mass at a velocity relative to Rocket. Fuel is ejecting at constant rate of . Initial Velocity rocket starts from rest from the surface of earth
( Neglect air and other resistance force in both Cases)
Q1). Assume gravity is constant , Find acceleration, velocity and Thrust as a function of time.
Q2). Assume gravity changes with height from earth surface as , Find acceleration, Velocity and Thrust as a function of time.
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Comments
Is acceleration M0−μtμu ?
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How do you find it ?? I don't know the answer.
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Use conservation of momentum and a=dv/dt.
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We can't apply conservation of momentum as there is gravity and also mass is changing with Time.
Use impulse momentum theoerem in both cases Consider any arbitrary moment in time t and distance y from surface of earth Let us consider that rocket as my system with mass at that point in spacetime as m In time dt let dm mass be ejected absolute velocity of dm is u-v where u is the relative velocity and v is the absolute velocity of rocket at that moment Impulse due to weight is mgdt which is the change in momentum of the system that is rocket After this we form a differentia equation which is dificult to solve in case 2 I am not able to solve the equation In case 1 V= uln(m■\m) -g\p(m■-m) Where m■ is initia mass p is dm\dt