A spaceship of mass m has velocity v in the positive x direction of an inertial reference
frame. A mass dm is fired out the rear of the ship with constant exhaust velocity (-v0) with
respect to the spaceship. a) using conservation of momentum, show that dv/v0 = dm/m, b)
By integration, find the dependence of v on m if v1 and m1 are the initial values. c) Can the
acceleration be constant if dm/dt, the burning rate is constant.
Given,
The mass of the spaceship be m and velocity be v.
a) So, initial momentum of the spaceship be
Now, as the dm mass fired from the spaceship, then also momentum always be conserve
b)
but here gravity is also working in downward direction,
c)
if dm/dt = constant
then
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