State the principle of rocket propulsion and obtain an expression for its acceleration and thrust on rocket. If in a rocket, fuel burns at a rate of 100 kgs and the exhaust gases are expelled out with a velocity 4.5 X 10 m/s. Calculate the force acting on the rocket
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Answer:
Relative velocity of exhaust gas V=2 km/s=2000 m/s
Thrust force F
t
=V
dt
dm
=2000×
dt
dm
Acceleration a=4.9 m/s
2
Mass of rocket M=1000 kg
Using Ma=F
t
−Mg
Or 1000×4.9=2000×
dt
dm
−1000×10
⟹
dt
dm
=7.35 kg/s
Explanation:
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