Answer:
a = 45 m/s/s
Explanation:
As we know that total mass of the rocket is
[tex]M = 6000 kg[/tex]
total mass of the fuel is given as
[tex]m = 2000 kg[/tex]
all the fuel is burnt in 15 s
so rate of the fuel burning is given as
[tex]\frac{dm}{dt} = \frac{2000}{15}[/tex]
[tex]\frac{dm}{dt} = 133.33 kg/s[/tex]
now the thrust force on the rocket is given as
[tex]F_{th} = v\frac{dm}{dt}[/tex]
[tex](6000 - 133.33 t) a = (900 + v)(133.33)[/tex]
so we have
[tex]\frac{dv}{900 + v} = (133.33)\frac{dt}{6000 - 133.33 t}[/tex]
so we have
[tex]ln(\frac{900 + v}{900}) = - ln(\frac{6000 - 133.3 t}{6000})[/tex]
[tex]1 + \frac{v}{900} = \frac{6000}{6000 - 133.3 t}[/tex]
now acceleration is rate of change in velocity
[tex]\frac{1}{900}\frac{dv}{dt} = \frac{133.3\times 6000}{(6000 - 133.3t)^2}[/tex]
so acceleration at t = 15 s
[tex]a = 45 m/s^2[/tex]