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A rocket of initial mass 6000kg ejects m...

A rocket of initial mass `6000kg` ejects mass at a constant rate of `16kg//s` with constant relative speed of `11m//s` What is the acceleration of the rocket one mnute after blast ?

A

`25"ms"^(-2)`

B

`50"ms"^(-2)`

C

`10"ms"^(-2)`

D

`35"ms"^(-2)`

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The correct Answer is:
To solve the problem of finding the acceleration of the rocket one minute after the blast, we can follow these steps: ### Step 1: Determine the initial mass of the rocket. The initial mass \( m_0 \) of the rocket is given as: \[ m_0 = 6000 \, \text{kg} \] ### Step 2: Calculate the mass of the rocket after one minute. The rocket ejects mass at a constant rate of \( \frac{dm}{dt} = 16 \, \text{kg/s} \). We need to find the total mass ejected in one minute (60 seconds): \[ \text{Mass ejected} = \frac{dm}{dt} \times \text{time} = 16 \, \text{kg/s} \times 60 \, \text{s} = 960 \, \text{kg} \] Now, we can find the mass of the rocket after one minute: \[ m = m_0 - \text{Mass ejected} = 6000 \, \text{kg} - 960 \, \text{kg} = 5040 \, \text{kg} \] ### Step 3: Determine the relative speed of the ejected mass. The relative speed \( V \) of the ejected mass is given as: \[ V = 11 \, \text{m/s} \] ### Step 4: Calculate the thrust force. The thrust force \( F \) generated by the rocket can be calculated using the formula: \[ F = \frac{dm}{dt} \times V \] Substituting the values: \[ F = 16 \, \text{kg/s} \times 11 \, \text{m/s} = 176 \, \text{N} \] ### Step 5: Calculate the acceleration of the rocket. Using Newton's second law, the acceleration \( a \) of the rocket can be calculated as: \[ a = \frac{F}{m} \] Substituting the thrust force and the mass of the rocket after one minute: \[ a = \frac{176 \, \text{N}}{5040 \, \text{kg}} \approx 0.0349 \, \text{m/s}^2 \] ### Step 6: Final Result Thus, the acceleration of the rocket one minute after the blast is approximately: \[ a \approx 0.0349 \, \text{m/s}^2 \]

To solve the problem of finding the acceleration of the rocket one minute after the blast, we can follow these steps: ### Step 1: Determine the initial mass of the rocket. The initial mass \( m_0 \) of the rocket is given as: \[ m_0 = 6000 \, \text{kg} \] ...
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