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A model rocket rests on a frictionless h...

A model rocket rests on a frictionless horizontal surface and is joined by a string of length `l` to a fixed point so that the rocket moves in a horizontal circular path of radius `l`. The string will break if its tensiion exceeds a value `T`. The rocket engine provides a thrust `F` of constant magnitude along the rocket's direction of motion. the rocket has a mass `m` that does not change with time. Answer the following questions based on the above passage.
What was the magnitude of instantaneous net acceleration at time `t_(1)//2`? Obtain answer in terms of `F, T` and `m`.

A

`([T^(2)+8F^(2)]^(1//2))/m`

B

`([T+4F^(2)]^(1//2))/(2m)`

C

`([T^(2)+16F^(2)]^(1//2))/(4m)`

D

none of these

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AI Generated Solution

The correct Answer is:
To solve the problem, we need to find the magnitude of the instantaneous net acceleration of the rocket at time \( t = \frac{t_1}{2} \). We will consider both the centripetal acceleration and the tangential acceleration due to the thrust provided by the rocket engine. ### Step-by-Step Solution: 1. **Identify the Forces Acting on the Rocket:** - The thrust \( F \) acts in the direction of the rocket's motion. - The tension \( T \) in the string provides the necessary centripetal force to keep the rocket moving in a circular path. 2. **Determine the Velocity of the Rocket at Time \( t = \frac{t_1}{2} \):** - The initial velocity \( u = 0 \) (the rocket starts from rest). - The acceleration \( a \) can be expressed as \( a = \frac{F}{m} \). - Using the equation of motion \( v = u + at \), we find: \[ v_1 = 0 + \left(\frac{F}{m}\right) \left(\frac{t_1}{2}\right) = \frac{F t_1}{2m} \] 3. **Calculate the Centripetal Acceleration \( a_c \):** - The centripetal acceleration is given by: \[ a_c = \frac{v^2}{r} \] - Substituting \( v_1 \) and \( r = l \): \[ a_c = \frac{\left(\frac{F t_1}{2m}\right)^2}{l} = \frac{F^2 t_1^2}{4m^2 l} \] 4. **Relate Tension to Centripetal Force:** - The tension \( T \) provides the centripetal force necessary for circular motion: \[ T = m a_c = m \left(\frac{F^2 t_1^2}{4m^2 l}\right) = \frac{F^2 t_1^2}{4m l} \] 5. **Determine the Tangential Acceleration \( a_t \):** - The tangential acceleration is simply given by: \[ a_t = \frac{F}{m} \] 6. **Calculate the Net Instantaneous Acceleration \( A \):** - The net acceleration is the vector sum of the centripetal and tangential accelerations: \[ A = \sqrt{a_c^2 + a_t^2} \] - Substituting the values we found: \[ A = \sqrt{\left(\frac{F^2 t_1^2}{4m^2 l}\right)^2 + \left(\frac{F}{m}\right)^2} \] - This simplifies to: \[ A = \sqrt{\frac{F^4 t_1^4}{16 m^4 l^2} + \frac{F^2}{m^2}} = \sqrt{\frac{F^2}{m^2} \left(\frac{F^2 t_1^4}{16 l^2} + 1\right)} \] - Therefore, the final expression for the instantaneous net acceleration is: \[ A = \frac{F}{m} \sqrt{\frac{F^2 t_1^4}{16 l^2} + 1} \] ### Final Answer: The magnitude of the instantaneous net acceleration at time \( t = \frac{t_1}{2} \) is: \[ A = \frac{F}{m} \sqrt{\frac{F^2 t_1^4}{16 l^2} + 1} \]

To solve the problem, we need to find the magnitude of the instantaneous net acceleration of the rocket at time \( t = \frac{t_1}{2} \). We will consider both the centripetal acceleration and the tangential acceleration due to the thrust provided by the rocket engine. ### Step-by-Step Solution: 1. **Identify the Forces Acting on the Rocket:** - The thrust \( F \) acts in the direction of the rocket's motion. - The tension \( T \) in the string provides the necessary centripetal force to keep the rocket moving in a circular path. ...
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