Answer:
h≅ 58 m
Step-by-step explanation:
GIVEN:
mass of rocket M= 62,000 kg
fuel consumption rate = 150 kg/s
velocity of exhaust gases v= 6000 m/s
Now thrust = rate of fuel consumption×velocity of exhaust gases
=6000 × 150 = 900000 N
now to need calculate time t = amount of fuel consumed÷ rate
= 744/150= 4.96 sec
applying newton's law
M×a= thrust - Mg
62000 a=900000- 62000×9.8
acceleration a= 4.71 m/s^2
its height after 744 kg of its total fuel load has been consumed
![h= (1)/(2)at^2](https://img.qammunity.org/2020/formulas/physics/college/ue319ykweeoli3s5fflh6f0p5rchkvnd9x.png)
![h= (1)/(2)4.71*4.96^2](https://img.qammunity.org/2020/formulas/physics/college/b4oa25t0p541wj91ueg8rdi4qh0cq1194j.png)
h= 58.012 m
h≅ 58 m