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 "(p)=mv"
Now, as the dm mass fired from the spaceship, then also momentum always be conserve
"\\frac{dp}{dt}=0"
"\\Rightarrow \\frac{d}{dt}(mv)=0"
"\\Rightarrow \\frac{dm}{dt}v+m\\frac{dv}{dt}=0"
"\\Rightarrow \\frac{dm}{dt}v=-\\frac{dv}{dt}m"
"\\frac{dm}{m}=-\\frac{dv}{v}"
b) "\\frac{dm}{dt}v+m\\frac{dv}{dt}"
but here gravity is also working in downward direction,
"\\int_{m_{1}}^{m-dm} \\frac{dm}{m}=\\int_{v_1}^v \\frac{dv}{v}"
"\\Rightarrow [\\ln m]_{m_1}^{m_1-dm}=[\\ln{v}]_{v_1}^v"
"\\Rightarrow \\ln[m_1-dm]-\\ln[m_1]=\\ln[v]-\\ln[v_1]"
"\\Rightarrow \\frac{m_1-dm}{m_1}=\\frac{v}{v_1}"
c)"m_1-dm=\\frac{v}{v_1}m_1"
"dm=m_1-\\frac{vm_1}{v_1}"
if dm/dt = constant
then "\\dfrac{dv}{dt}=-g+k\\frac{v'}{m}"
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