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A rocket of mass 20kg has 180kg fuel. Th...

A rocket of mass `20kg` has `180kg` fuel. The exhaust velocity of the fuel is `1.6km//s`. Calculate the minimum rate of consumption of fuel so that the rocket may rise from the ground. Also, calculate the ultimate vertical speed gained by the rocket when the rate of consumption of fuel is `(g=9.8m//s^2)`
(i) `2kg//s` (ii) `20kg//s`

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To solve the problem step-by-step, we will break it down into parts. ### Given Data: - Mass of the rocket (m_rocket) = 20 kg - Mass of the fuel (m_fuel) = 180 kg - Total mass (m_0) = m_rocket + m_fuel = 20 kg + 180 kg = 200 kg - Exhaust velocity (V_r) = 1.6 km/s = 1600 m/s - Acceleration due to gravity (g) = 9.8 m/s² ### Part 1: Minimum Rate of Consumption of Fuel 1. **Calculate the weight of the rocket**: \[ W = m_0 \cdot g = 200 \, \text{kg} \cdot 9.8 \, \text{m/s}^2 = 1960 \, \text{N} \] 2. **Establish the thrust force (F_t)**: The thrust force must equal the weight of the rocket for it to just rise: \[ F_t = W \] 3. **Relate thrust force to rate of fuel consumption**: The thrust force can also be expressed as: \[ F_t = V_r \cdot \left(-\frac{dm}{dt}\right) \] where \(-\frac{dm}{dt}\) is the rate of fuel consumption. 4. **Set the equations equal**: \[ V_r \cdot \left(-\frac{dm}{dt}\right) = W \] Rearranging gives: \[ -\frac{dm}{dt} = \frac{W}{V_r} \] 5. **Substitute known values**: \[ -\frac{dm}{dt} = \frac{1960 \, \text{N}}{1600 \, \text{m/s}} = 1.225 \, \text{kg/s} \] Therefore, the minimum rate of consumption of fuel is: \[ \frac{dm}{dt} \approx 1.225 \, \text{kg/s} \] ### Part 2: Ultimate Vertical Speed for Different Rates of Consumption #### (i) For a rate of consumption of fuel = 2 kg/s 1. **Calculate the time until fuel is exhausted**: \[ T = \frac{m_fuel}{\text{Rate of consumption}} = \frac{180 \, \text{kg}}{2 \, \text{kg/s}} = 90 \, \text{s} \] 2. **Calculate the final mass when fuel is exhausted**: \[ m = m_0 - m_fuel = 200 \, \text{kg} - 180 \, \text{kg} = 20 \, \text{kg} \] 3. **Use the formula for ultimate vertical speed**: \[ V = u - gT + V_r \cdot \ln\left(\frac{m_0}{m}\right) \] where \(u = 0\) (initial velocity). 4. **Substituting the values**: \[ V = 0 - 9.8 \cdot 90 + 1600 \cdot \ln\left(\frac{200}{20}\right) \] \[ V = -882 + 1600 \cdot \ln(10) \] \[ V \approx -882 + 1600 \cdot 2.302 \approx -882 + 3683.2 \approx 2801.2 \, \text{m/s} \] #### (ii) For a rate of consumption of fuel = 20 kg/s 1. **Calculate the time until fuel is exhausted**: \[ T = \frac{180 \, \text{kg}}{20 \, \text{kg/s}} = 9 \, \text{s} \] 2. **Calculate the final mass when fuel is exhausted**: \[ m = 200 \, \text{kg} - 180 \, \text{kg} = 20 \, \text{kg} \] 3. **Use the same formula for ultimate vertical speed**: \[ V = 0 - 9.8 \cdot 9 + 1600 \cdot \ln\left(\frac{200}{20}\right) \] \[ V = -88.2 + 1600 \cdot 2.302 \approx -88.2 + 3683.2 \approx 3595 \, \text{m/s} \] ### Final Answers: 1. Minimum rate of consumption of fuel: **1.225 kg/s** 2. Ultimate vertical speed for 2 kg/s: **2801.2 m/s** 3. Ultimate vertical speed for 20 kg/s: **3595 m/s**

To solve the problem step-by-step, we will break it down into parts. ### Given Data: - Mass of the rocket (m_rocket) = 20 kg - Mass of the fuel (m_fuel) = 180 kg - Total mass (m_0) = m_rocket + m_fuel = 20 kg + 180 kg = 200 kg - Exhaust velocity (V_r) = 1.6 km/s = 1600 m/s - Acceleration due to gravity (g) = 9.8 m/s² ...
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Knowledge Check

  • The force on a rocket moving with a veloctiy 300 m/s is 210N. The rate of consumption of fuel of rocket is

    A
    `0.07 kg s^(-1)`
    B
    `1.4kg s^(-1)`
    C
    `0.7kg s^(-1)`
    D
    `10.7kg s^(-1)`
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