A rocket motor consume 100 kg of fuel per second, exhausting it with a speed of 6 x 104 ms. What thrust is exerted the rocket ? What will be the velocity of rocket at the instant its mass is reduced (1/40)th of its initial mass ? Take initial velocit of rocket as zero. Neglect gravity. Dm
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=> Here, A rocket motor consume 100 kg of fuel per second, exhausting it with a speed of 6 x 104 ms.
∴ dm/dt = 100kg/s
u = 6* 10⁴ m/s
Thus, Thrust F = u*dm/dt = 6*10⁴*100
= 6×10⁶ N
(ii) The velocity of rocket when its mass is reduced (1/40)th at the instant of its initial mass:
Here, m= 1/40 * m₀
m₀/m = 40
velocity, υ = (2.303)u log₁₀ (m₀/m)
= 2.303 × 6 × 10⁴ × log₁₀ 40
= 2.303 × 6 ×10⁴ ×1.602
= 22.13×10⁴ m/s .
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