In a rocket of mass 1000 kg fuel is consumed at a rate of 40 kg/s. the velocity of the gases ejected from the rocket is 50000 m/s. the thrust on the rocket is
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Answered by
148
heya!
thrust force = Vrel × (dm/dt)
here Vrel = 5 × 10⁴m/s
Ft = 5 × 10⁴ × 40
= 2 × 10^6N ans
easy peasy hope i answered it correctly ..^_^
thrust force = Vrel × (dm/dt)
here Vrel = 5 × 10⁴m/s
Ft = 5 × 10⁴ × 40
= 2 × 10^6N ans
easy peasy hope i answered it correctly ..^_^
Answered by
2
Answer:
2 × 10 ^ 6 N is correct answers of this question
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