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A rocket of mass1000kg exhaust gases at the rate of 4 kg/s with a velocity 3000 m/s.the thrust developed on the rocket?
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A rocket of mass1000kg exhaust gases at the rate of 4 kg/s with a velo...
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A rocket of mass1000kg exhaust gases at the rate of 4 kg/s with a velo...
The thrust developed by the rocket can be calculated using the formula:
Thrust = Rate of change of momentum
- Given data:
- Mass of the rocket (m) = 1000 kg
- Rate of exhaust of gases (dm/dt) = 4 kg/s
- Velocity of exhaust gases (v) = 3000 m/s
- Calculating the rate of change of momentum:
- Rate of change of momentum = dm/dt * v
- Rate of change of momentum = 4 kg/s * 3000 m/s
- Rate of change of momentum = 12000 N
- Thrust developed by the rocket:
- Thrust = Rate of change of momentum
- Thrust = 12000 N
Therefore, the thrust developed by the rocket is 12000 N. This means that the rocket is producing a force of 12000 N in the opposite direction of the exhaust gases to propel itself forward.
Thrust = Rate of change of momentum
- Given data:
- Mass of the rocket (m) = 1000 kg
- Rate of exhaust of gases (dm/dt) = 4 kg/s
- Velocity of exhaust gases (v) = 3000 m/s
- Calculating the rate of change of momentum:
- Rate of change of momentum = dm/dt * v
- Rate of change of momentum = 4 kg/s * 3000 m/s
- Rate of change of momentum = 12000 N
- Thrust developed by the rocket:
- Thrust = Rate of change of momentum
- Thrust = 12000 N
Therefore, the thrust developed by the rocket is 12000 N. This means that the rocket is producing a force of 12000 N in the opposite direction of the exhaust gases to propel itself forward.
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A rocket of mass1000kg exhaust gases at the rate of 4 kg/s with a velocity 3000 m/s.the thrust developed on the rocket?
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A rocket of mass1000kg exhaust gases at the rate of 4 kg/s with a velocity 3000 m/s.the thrust developed on the rocket? for NEET 2024 is part of NEET preparation. The Question and answers have been prepared according to the NEET exam syllabus. Information about A rocket of mass1000kg exhaust gases at the rate of 4 kg/s with a velocity 3000 m/s.the thrust developed on the rocket? covers all topics & solutions for NEET 2024 Exam. Find important definitions, questions, meanings, examples, exercises and tests below for A rocket of mass1000kg exhaust gases at the rate of 4 kg/s with a velocity 3000 m/s.the thrust developed on the rocket?.
A rocket of mass1000kg exhaust gases at the rate of 4 kg/s with a velocity 3000 m/s.the thrust developed on the rocket? for NEET 2024 is part of NEET preparation. The Question and answers have been prepared according to the NEET exam syllabus. Information about A rocket of mass1000kg exhaust gases at the rate of 4 kg/s with a velocity 3000 m/s.the thrust developed on the rocket? covers all topics & solutions for NEET 2024 Exam. Find important definitions, questions, meanings, examples, exercises and tests below for A rocket of mass1000kg exhaust gases at the rate of 4 kg/s with a velocity 3000 m/s.the thrust developed on the rocket?.
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