Question

2. Fuel is consumed at the rate of 50 g per second in a
rocket. The exhaust gases are rejected at the rate of
5x10^5 cm/s ? What is the thrust experienced by the
rocket?
(Ans. 250 N)​

Answer 1

Answer:

250 N

Explanation:

F = ma

m=0.05

a = 5 * 10^3 m/s^2

F = 0.05 * 5*10^3 = 250 N = thrust

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