One of the waste products of a nuclear reactor is plutonium\( - 239\left( {^{239}Pu} \right)\). This nucleus is radioactive and decays by splitting into a helium-\(4\)nucleus and a uranium\( - 235\)nucleus\(\left( {^4He{ + ^{235}}U} \right)\), the latter of which is also radioactive and will itself decay some time later. The energy emitted in the plutonium decay is\(8.40 \times 1{0^{ - 13}}\;J\)and is entirely converted to kinetic energy of the helium and uranium nuclei. The mass of the helium nucleus is\(6.68 \times 1{0^{ - 27}}kg\),while that of the uranium is\(3.92 \times 1{0^{ - 25}}\;kg\)(note that the ratio of the masses is\(4\)to\(235\)). (a) Calculate the velocities of the two nuclei, assuming the plutonium nucleus is originally at rest. (b) How much kinetic energy does each nucleus carry away? Note that the data given here are accurate to three digits only.

Short Answer

Expert verified

(a) The velocity of the helium atom after explosion is \( - 1.57 \times 1{0^7}\,m/s\). The velocity of the uranium atom is \(2.68\, \times 1{0^5}m/s\).

(b) The kinetic energy of uranium atom is \(1.41 \times 1{0^{ - 14}}J\)

Step by step solution

01

Definition of Kinetic Energy

Kinetic energy is the energy that an item or particle has as a result of its movement. When work is done on an object by exerting a net force, the object accelerates and gains kinetic energy as a result.

02

Given data

The mass of the helium nuclei is \({M_{He}} = 6.68 \times 1{0^{ - 27}}kg\)

The mass of the uranium nuclei is \({M_U} = 3.92 \times 1{0^{ - 25}}\;kg\)

The velocity of the helium and uranium nuclei before decay \({U_{He}} = {U_U} = 0 m/s\)

03

Velocity of the nuclei after collision

By putting all the value into the equation we get

\(\begin{aligned}{M_p}{V_p} &= {M_{He}}{V_{He}} + {M_U}{V_{Ua}}\\\cancel{{{M_p}{V_p}}} &= {M_{He}}{V_{He}} + {M_U}{V_{Ua}}\\ - {M_{He}}{V_{He}} &= {M_U}{V_{Ua}}\end{aligned}\)…………………(1)

The above equation we can use in kinetic energy equation.

\(\begin{aligned}K{E_{in}} &= K{E_f} - K{E_i}\\K{E_{in}} &= \left( {K{E_{He}} + K{E_U}} \right) - \cancel{{K{E_i}}}\\K{E_{in}} &= \left( {\dfrac{1}{2}{m_{He}}{v_{He}}^2 + \dfrac{1}{2}{m_u}{v_{Ua}}^2} \right) - 0\\K{E_{in}} &= \dfrac{1}{2}\left( {{m_{He}}{v_{He}}^2 + {m_u}{{\left( {\dfrac{{ - {m_{He}}{v_{He}}}}{{{m_u}}}} \right)}^2}} \right)....from\,eq\,(1)\end{aligned}\)

\(\begin{aligned}2K{E_{in}} &= {m_U}{v_U}^2 + \dfrac{{{m_{}}^2{v_{1a}}^2}}{{{m_2}}}\\2K{E_{in}} &= {v_{He}}^2\left( {{m_{He}} + \dfrac{{{m_{He}}^2}}{{{m_u}}}} \right)\end{aligned}\)

\(\begin{aligned}{v_{He}} &= \sqrt {\dfrac{{2K{E_{in}}}}{{\left( {{m_{He}} + \dfrac{{{m_{He}}^2}}{{{m_U}}}} \right)}}} \\{v_{He}} &= \sqrt {\dfrac{{2\left( {8.4 \times 1{0^{ - 13}}} \right)}}{{\left( {6.68 \times 1{0^{ - 27}} + \dfrac{{{{\left( {6.68 \times 1{0^{ - 27}}} \right)}^2}}}{{3.92 \times 1{0^{ - 25}}}}} \right)}}} \\{v_{He}} &= \pm 1.57 \times 1{0^7}\,m/s\\{v_{He}} &= - 1.57 \times 1{0^7}\,m/s\end{aligned}\)

Hence the velocity of the helium atom after explosion is \( - 1.57 \times 1{0^7}\,m/s\)

04

Value of uranium atom velocity

Putting the value of the velocity in equation 1

\(\begin{aligned} - {M_{He}}{V_{He}} &= {M_U}{V_{Ua}}\\{V_{Ua}} &= \dfrac{{ - {M_{He}}{V_{He}}}}{{{M_U}}}\\{V_{Ua}} &= \dfrac{{ - \left( {6.68 \times 1{0^{ - 27}}} \right)\left( {1.57 \times 1{0^7}} \right)}}{{\left( {3.92 \times 1{0^{ - 25}}} \right)}}\\{V_{Ua}} &= 2.68\, \times 1{0^5}m/s\end{aligned}\)

Therefore, the velocity of the uranium atom is \(2.68\, \times 1{0^5}m/s\)

05

Step 5:Kinetic energy each nucleus carries away

The kinetic energy does each nucleus carry away

\(\begin{aligned}K{E_{He}} &= \dfrac{1}{2}m{V^2}\\ &= \dfrac{1}{2}\left( {6.68x1{0^{ - 27}}} \right){\left( {1.57x1{0^7}} \right)^2}\\ &= 8.23 \times 1{0^{ - 13}}\end{aligned}\)

The kinetic energy of Helium atom is \(8.23 \times 1{0^{ - 13}}\)

Similarly for the uranium atom it will be

\(\begin{aligned}K{E_U} &= \dfrac{1}{2}m{V^2}\\ &= \dfrac{1}{2}\left( {3.92x1{0^{ - 25}}} \right){\left( {2.68x1{0^5}} \right)^2}\\ &= 1.41 \times 1{0^{ - 14}}J\end{aligned}\)

Therefore, the kinetic energy of uranium atom is \(1.41 \times 1{0^{ - 14}}J\)

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Most popular questions from this chapter

Ernest Rutherford (the first New Zealander to be awarded the Nobel rize in Chemistry) demonstrated that nuclei were very small and dense by scattering helium-4 nuclei\(\left( {{}^4He} \right)\)from gold-197 nuclei\(\left( {{}^{197}Au} \right)\).The energy of the incoming helium nucleus was\(8.00 \times {10^{ - 13}}\;{\rm{J}}\), and themasses of the helium and gold nuclei were\(6.68 \times {10^{ - 27}}\;{\rm{kg}}\)and\(3.29 \times {10^{ - 25}}\;{\rm{kg}}\), respectively (note that their mass ratio is 4 to 197). (a) If a helium nucleus scatters to an angle of\(120^\circ \)during an elastic collision with a gold nucleus, calculate the helium nucleus’s final speed and the final velocity (magnitude and direction) of the gold nucleus. (b) What is the final kinetic energy of the helium nucleus?

A\(5.50\;kg\)bowling ball moving at\(9.00\;{\rm{m/s}}\)collides with a\(0.850\;{\rm{kg}}\)bowling pin, which is scattered at an angle of\(85.{0^ \circ }\)to the initial direction of the bowling ball and with a speed of\(15.0\;{\rm{m/s}}\). (a) Calculate the final velocity (magnitude and direction) of the owling ball. (b) Is the collision elastic? (c) Linear kinetic energy is greater after the collision. Discuss how spin on the ball might be converted to linear kinetic energy in the collision.

Antiballistic missiles (ABMs) are designed to have very large accelerations so that they may intercept fast-moving incoming missiles in the short time available. What is the takeoff acceleration of a \(10,000\;kg\) ABM that expels \(196\;kg\) of gas per second at an exhaust velocity of\(2.50 \times {10^3}\;kg\)?

It is possible for the velocity of a rocket to be greater than the exhaust velocity of the gases it ejects. When that is the case, the gas velocity and gas momentum are in the same direction as that of the rocket. How is the rocket still able to obtain thrust by ejecting the gases?

Ion-propulsion rockets have been proposed for use in space. They employ atomic ionization techniques and nuclear energy sources to produce extremely high exhaust velocities, perhaps as great as\(8.00 \times {10^6}\;m/s\). These techniques allow a much more favorable payload-to-fuel ratio. To illustrate this fact: (a) Calculate the increase in velocity of a\(20000\;kg\)space probe that expels only\(40.0\;kg\)of its mass at the given exhaust velocity. (b) These engines are usually designed to produce a very small thrust for a very long time—the type of engine that might be useful on a trip to the outer planets, for example. Calculate the acceleration of such an engine if it expels\(4.50 \times {10^6}\;kg/s\) at the given velocity, assuming the acceleration due to gravity is negligible.

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