The rocket initial mass is 100 kg. The rocket mass after burnout is 40 kg. Rocket propellant burnt for 5 seconds. The
Specific impulse of the rocket engine is 200 seconds. Then Thrust in N by considering the rocket is flying inside the
earth of constant gravity field and correctly expanded flow pattern
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Rocket propellant burnt for 5 seconds. The
Specific impulse of the rocket engine is 200 seconds. Then Thrust in N by considering the rocket is flying inside the
earth of constant gravity field and correctly
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