Let R be the constant upward thrust on the aerostat of mass m, coming down with a constant acceleration w. Applying Newton's second law of motion for the aerostat in projection form
Fy=mwy
mg−R=mw (1)
Now, if Δm be the mass, to be dumped, then using the equation Fy=mwy
R−(m−Δm)g=(m−Δm)w, (2)
From equations (1) and (2), we get, Δm=2mwg+w