Chapter 9 Linear Momentum and Collisions
The momentum \(\vec{p}\) of an object is the product of its mass (\(m\)) and its velocity (\(\vec{v}\)):
\[\vec{p} = m\vec{v}\]
Momentum is a vector quantity because velocity is a vector.
Caption: The velocity and momentum vectors for the ball are in the same direction. (credit: modification of work by Ben Sutherland)
Caption: Supertanker
Caption: Gas molecules
Note
These momenta differ by 27 orders of magnitude! Momentum depends equally on mass and velocity.
Caption: Change in momentum is proportional to the time the force is applied.
The product of a force and the time interval over which it acts is called impulse (\(\vec{J}\)).
For a differential time interval \(dt\): \[d\vec{J} \equiv \vec{F}(t)dt\]
Total impulse over an interval \(t_f - t_i\): \[\vec{J} \equiv \int_{t_i}^{t_f}\vec{F}(t)dt\]
Caption: A force applied by a tennis racquet to a tennis ball over a time interval generates an impulse acting on the ball.
If we don’t know the force function \(F(t)\), we can use the average force \(\vec{F}_{ave}\). \[\vec{F}_{ave} = \frac{1}{\Delta t} \int_{t_i}^{t_f}\vec{F}(t)dt\]
Therefore, impulse can also be expressed as: \[\vec{J} = \vec{F}_{ave}\Delta t\]
This means you only need the average force to calculate impulse.
Starting with \(F(t) = ma(t)\): \[\vec{J} = \int_{t_i}^{t_f}\vec{F}(t)dt = \int_{t_i}^{t_f} m\vec{a}(t)dt\]
Since \(\vec{a}(t) = \frac{d\vec{v}}{dt}\): \[\vec{J} = m\int_{t_i}^{t_f} \frac{d\vec{v}}{dt}dt = m[\vec{v}(t_f) - \vec{v}(t_i)]\]
For constant force \(\vec{F}_{ave} = \vec{F} = m\vec{a}\): \[\vec{J} = m\vec{a}\Delta t = m\vec{v}_f - m\vec{v}_i = m(\vec{v}_f - \vec{v}_i)\]
Impulse-Momentum Theorem
An impulse applied to a system changes the system’s momentum, and that change of momentum is exactly equal to the impulse that was applied:
\[\vec{J} = \Delta\vec{p}\]
Caption: Illustration of impulse-momentum theorem.
Caption: Arizona Meteor Crater.
Strategy:
Mass of meteor:
\(V = \frac{4}{3}\pi R^3 = \frac{4}{3}\pi (25 \text{ m})^3 = 6.54 \times 10^4 \text{ m}^3\)
\(m = \rho V = (7970 \text{ kg/m}^3)(6.54 \times 10^4 \text{ m}^3) = 5.21 \times 10^8 \text{ kg}\)
Average force:
\(\vec{F}_{ave} = \frac{m\Delta\vec{v}}{\Delta t}\)
Initial velocity: \(\vec{v}_i = -(1.28 \times 10^4 \text{ m/s})\hat{j}\)
Final velocity: \(\vec{v}_f = 0\)
Assumed impact time: \(\Delta t = 2 \text{ s}\)
\(\vec{F}_{ave} = \frac{(5.21 \times 10^8 \text{ kg})(0 - (-1.28 \times 10^4 \text{ m/s}))\hat{j}}{2 \text{ s}} = +(3.33 \times 10^{12} \text{ N})\hat{j}\)
Maximum force (using \(F(t) = F_{max}e^{-t^2/(2\tau^2)}\)):
We found \(F_{ave} = 3.33 \times 10^{12} \text{ N}\).
Given \(\Delta t = t_{max} - 0 \text{ s} = 2 \text{ s}\).
Integral of \(F(t)\) over \(\Delta t\):
\(\int_{0}^{t_{max}} F_{max}e^{-t^2/(2\tau^2)}dt\)
Choosing \(\tau = \frac{1}{e} t_{max}\), the integral gives \(F_{ave} = 0.458 F_{max}\).
\(F_{max} = \frac{F_{ave}}{0.458} = \frac{3.33 \times 10^{12} \text{ N}}{0.458} = 7.27 \times 10^{12} \text{ N}\)
Force on Earth by meteor:
\(\vec{F}_{meteor}(t) = -(7.27 \times 10^{12} \text{ N})e^{-t^2/(8\text{s}^2)}\hat{j}\)
Caption: Graph of the average force (red) and instantaneous force (blue) during impact.
Important
Airbags and seatbelts drastically reduce the average force on occupants by increasing the collision time (\(\Delta t\)). The change in momentum (\(\Delta p\)) is the same in both cases.
Average force: \(\vec{F}_{ave} = \frac{\Delta\vec{p}}{\Delta t}\)
For a continuously changing momentum (\(\Delta t \to dt\)):
\[\vec{F} = \frac{d\vec{p}}{dt}\]
This is Newton’s second law expressed in terms of momentum.
If mass is constant, \(\vec{F} = \frac{d(m\vec{v})}{dt} = m\frac{d\vec{v}}{dt} = m\vec{a}\).
This form is particularly useful when the mass of the system changes, like in rocket propulsion.
Newton’s Second Law of Motion in Terms of Momentum
The net external force on a system is equal to the rate of change of the momentum of that system caused by the force:
\[\vec{F}_{net} = \frac{d\vec{p}}{dt}\]
Calculate the average force on a tennis ball during Venus Williams’ serve.
Strategy:
Solution:
\(\Delta p = (0.057 \text{ kg})(58 \text{ m/s} - 0 \text{ m/s}) = 3.3 \text{ kg} \cdot \text{m/s}\)
\(F = \frac{3.3 \text{ kg} \cdot \text{m/s}}{5.0 \times 10^{-3} \text{ s}} = 6.6 \times 10^2 \text{ N}\)
Generalizing to \(N\) objects:
\[\vec{p}_1 + \vec{p}_2 + \dots + \vec{p}_N = \text{constant}\]
\[\sum_{j=1}^{N}\vec{p}_j = \text{constant}\]
If a physical quantity is constant in time, it is conserved.
Caption: Total momentum of the system before and after a collision remains the same.
For a system’s momentum to be conserved, it must be a closed system (also called an isolated system), meeting two requirements:
Law of Conservation of Momentum
The total momentum of a closed system is conserved:
\[\sum_{j=1}^{N}\vec{p}_j = \text{constant}\]
Caption: The two cars together form the system that is to be analyzed.
Cart 1: \(m_1 = 675 \text{ g} = 0.675 \text{ kg}\), \(v_{1i} = 0.75 \text{ m/s}\) (right)
Cart 2: \(m_2 = 500 \text{ g} = 0.500 \text{ kg}\), \(v_{2i} = 1.33 \text{ m/s}\) (right)
Carts stick together after collision. Find final velocity \(v_f\).
Strategy:
Solution: Define right as \(+x\). Initial momentum: \(\vec{p}_i = m_1\vec{v}_{1i} + m_2\vec{v}_{2i} = (0.675)(0.75)\hat{i} + (0.500)(1.33)\hat{i}\) Final momentum: \(\vec{p}_f = (m_1+m_2)\vec{v}_f = (0.675+0.500)\vec{v}_f\)
\((0.675+0.500)\vec{v}_f = (0.675)(0.75)\hat{i} + (0.500)(1.33)\hat{i}\) \(1.175\vec{v}_f = (0.50625 + 0.665)\hat{i}\) \(\vec{v}_f = \frac{1.17125}{1.175}\hat{i} = (0.997 \text{ m/s})\hat{i}\)
Collision Types and Kinetic Energy
Proton (\(m_p = 1.67 \times 10^{-27} \text{ kg}\)) collides with a neutron (\(m_n \approx m_p\)) to form a deuteron.
Proton velocity: \(v_p = 7.0 \times 10^6 \text{ m/s}\) (right).
Neutron velocity: \(v_n = 4.0 \times 10^6 \text{ m/s}\) (left).
Find the velocity of the deuteron (\(v_d\)).
Strategy:
Solution: Initial momentum: \(p_i = Mv_p - Mv_n\) Final momentum: \(p_f = (M+M)v_d = 2Mv_d\)
\(Mv_p - Mv_n = 2Mv_d\) \(v_p - v_n = 2v_d\) \((7.0 \times 10^6 \text{ m/s}) - (4.0 \times 10^6 \text{ m/s}) = 2v_d\) \(3.0 \times 10^6 \text{ m/s} = 2v_d\) \(v_d = 1.5 \times 10^6 \text{ m/s}\) (to the right) \(\vec{v}_d = (1.5 \times 10^6 \text{ m/s})\hat{i}\)
Red puck: \(m_1 = 15 \text{ g} = 0.015 \text{ kg}\), \(v_{1i} = 0 \text{ m/s}\).
Blue puck: \(m_2 = 12 \text{ g} = 0.012 \text{ kg}\), \(v_{2i} = 2.5 \text{ m/s}\) (left).
Collision is perfectly elastic. Find final velocities \(v_{1f}\) and \(v_{2f}\).
Strategy:
Solution: Define left as \(+x\).
Conservation of Momentum: \(m_2v_{2i} = m_1v_{1f} + m_2v_{2f}\) \((0.012)(2.5) = (0.015)v_{1f} + (0.012)v_{2f}\) \(0.030 = 0.015v_{1f} + 0.012v_{2f}\) (Eq. 1)
Conservation of Kinetic Energy: \(\frac{1}{2}m_2v_{2i}^2 = \frac{1}{2}m_1v_{1f}^2 + \frac{1}{2}m_2v_{2f}^2\) \((0.012)(2.5)^2 = (0.015)v_{1f}^2 + (0.012)v_{2f}^2\) \(0.075 = 0.015v_{1f}^2 + 0.012v_{2f}^2\) (Eq. 2)
Solving these simultaneous equations (tedious but possible): \(v_{1f} = 2.22 \text{ m/s}\) (left) \(v_{2f} = -0.28 \text{ m/s}\) (right)
Car: \(m_c = 1200 \text{ kg}\), \(v_c = 60 \text{ km/hr}\) (East)
Truck: \(m_T = 3000 \text{ kg}\), \(v_T = 40 \text{ km/hr}\) (North)
Vehicles lock together (perfectly inelastic collision). Find final velocity of wreckage \(\vec{v}_w\).
Strategy:
Solution: Initial momentum: \(\vec{p}_i = m_c\vec{v}_c + m_T\vec{v}_T\) Final momentum: \(\vec{p}_f = (m_c+m_T)\vec{v}_w\) \(\vec{p}_i = \vec{p}_f \implies m_c\vec{v}_c + m_T\vec{v}_T = (m_c+m_T)\vec{v}_w\)
x-direction: \(m_c v_c = (m_c+m_T)v_{w,x}\) \(v_{w,x} = \frac{m_c}{m_c+m_T}v_c = \frac{1200}{1200+3000}(16.67) = \frac{1200}{4200}(16.67) = 4.76 \text{ m/s}\)
y-direction: \(m_T v_T = (m_c+m_T)v_{w,y}\) \(v_{w,y} = \frac{m_T}{m_c+m_T}v_T = \frac{3000}{1200+3000}(11.11) = \frac{3000}{4200}(11.11) = 7.94 \text{ m/s}\)
Magnitude of \(\vec{v}_w\): \(|\vec{v}_w| = \sqrt{v_{w,x}^2 + v_{w,y}^2} = \sqrt{(4.76)^2 + (7.94)^2} = \sqrt{22.66 + 63.04} = \sqrt{85.7} \approx 9.26 \text{ m/s}\) (\(9.26 \text{ m/s} \approx 33.3 \text{ km/hr}\))
Direction of \(\vec{v}_w\): \(\theta = \tan^{-1}\left(\frac{v_{w,y}}{v_{w,x}}\right) = \tan^{-1}\left(\frac{7.94}{4.76}\right) = \tan^{-1}(1.668) \approx 59.1^\circ\) North of East.
Caption: As the cat falls, its body performs complicated motions so it can land on its feet, but one point in the system moves with the simple uniform acceleration of gravity.
Note
The total change of momentum of the entire object is due only to the external forces. Internal forces do not change the momentum of the object as a whole.
The total momentum of the system is \(\vec{p}_{CM} = \sum_{j=1}^{N} \vec{p}_j\).
Newton’s second law for the system: \(\vec{F}_{ext} = \frac{d\vec{p}_{CM}}{dt}\).
To relate this to acceleration, we define the center of mass: \[\vec{r}_{CM} \equiv \frac{1}{M}\sum_{j=1}^{N}m_j\vec{r}_j\] Where \(M = \sum_{j=1}^{N} m_j\) is the total mass.
The center of mass is the point in the object that obeys Newton’s second law for the system: \[\vec{F}_{ext} = M\vec{a}_{CM}\] Where \(\vec{a}_{CM} = \frac{d^2\vec{r}_{CM}}{dt^2}\).
Important
There does not have to be any actual mass at the center of mass of an object (e.g., a hollow sphere, a donut).
The center of mass can be calculated for each component independently:
\[x_{CM} = \frac{1}{M}\sum_{j=1}^{N}m_jx_j\]
\[y_{CM} = \frac{1}{M}\sum_{j=1}^{N}m_jy_j\]
\[z_{CM} = \frac{1}{M}\sum_{j=1}^{N}m_jz_j\]
The position vector is \(\vec{r}_{CM} = x_{CM}\hat{i} + y_{CM}\hat{j} + z_{CM}\hat{k}\).
Instantaneous velocity of the center of mass:
\[\vec{v}_{CM} = \frac{d\vec{r}_{CM}}{dt} = \frac{1}{M}\sum_{j=1}^{N}m_j\vec{v}_j\]
Acceleration of the center of mass: \[\vec{a}_{CM} = \frac{d\vec{v}_{CM}}{dt} = \frac{1}{M}\sum_{j=1}^{N}m_j\vec{a}_j = \frac{\vec{F}_{ext}}{M}\]
\(m_e = 5.97 \times 10^{24} \text{ kg}\)
\(m_m = 7.36 \times 10^{22} \text{ kg}\)
Distance \(r_m = 3.82 \times 10^8 \text{ m}\) (center to center)
Strategy:
Solution:
\(R = \frac{(5.97 \times 10^{24} \text{ kg})(0 \text{ m}) + (7.36 \times 10^{22} \text{ kg})(3.82 \times 10^8 \text{ m})}{5.97 \times 10^{24} \text{ kg} + 7.36 \times 10^{22} \text{ kg}}\)
\(R = \frac{2.812 \times 10^{31}}{6.0436 \times 10^{24}} = 4.64 \times 10^6 \text{ m}\)
Significance:
Find the center of mass of a uniform thin hoop of mass \(M\) and radius \(r\).
Strategy:
Solution:
\(\vec{r}_{CM} = \frac{1}{M}\int_{0}^{2\pi} [(r\cos\theta)\hat{i} + (r\sin\theta)\hat{j}] (\lambda r d\theta)\)
\(\vec{r}_{CM} = \frac{1}{M}\int_{0}^{2\pi} [(r\cos\theta)\hat{i} + (r\sin\theta)\hat{j}] \left(\frac{M}{2\pi r}\right) r d\theta\)
\(\vec{r}_{CM} = \frac{1}{2\pi}\int_{0}^{2\pi} [(r\cos\theta)\hat{i} + (r\sin\theta)\hat{j}] d\theta\)
\(x_{CM} = \frac{r}{2\pi}\int_{0}^{2\pi} \cos\theta d\theta = \frac{r}{2\pi}[\sin\theta]_{0}^{2\pi} = 0\)
\(y_{CM} = \frac{r}{2\pi}\int_{0}^{2\pi} \sin\theta d\theta = \frac{r}{2\pi}[-\cos\theta]_{0}^{2\pi} = 0\)
\(\vec{r}_{CM} = 0\hat{i} + 0\hat{j} = \vec{0}\)
As expected, the center of mass is at the origin (geometric center).
For a system of \(N\) objects, the velocity of the center of mass is:
\[\vec{v}_{CM} = \frac{1}{M}\sum_{j=1}^{N}m_j\vec{v}_j\]
This also means \(M\vec{v}_{CM} = \sum_{j=1}^{N}m_j\vec{v}_j = \vec{P}_{total}\).
Conservation of momentum implies:
\(M\vec{v}_{CM,f} = M\vec{v}_{CM,i}\)
Therefore, \(\vec{v}_{CM,f} = \vec{v}_{CM,i}\)
In the absence of an external force, the velocity of the center of mass never changes.
This applies to a vast collection of interacting particles, even if individual particles’ momenta change!
Caption: Exploding fireworks are a vivid example of conservation of momentum and the motion of the center of mass.
Caption: Rocket accelerating due to expulsion of fuel.
Consider a system of rocket + fuel in deep space (no external forces).
At time \(t\), rocket has mass \(m\) and velocity \(v\).
During \(dt\), it ejects mass \(dm_g\) (fuel) at velocity \(u\) (relative to rocket) in the \(-x\) direction.
Rocket’s mass becomes \(m-dm_g\), velocity becomes \(v+dv\).
Momentum conservation: \(mv = (m-dm_g)(v+dv) + dm_g(v-u)\)
Simplifying and noting \(dm_g = -dm\) (decrease in rocket mass): \(mdv = -dm \cdot u\) \(dv = -u \frac{dm}{m}\)
Integrating from initial mass \(m_0\) to final mass \(m\): \[\int_{v_i}^{v_f} dv = -u\int_{m_0}^{m} \frac{dm}{m}\] \[\Delta v = v_f - v_i = u \ln\left(\frac{m_0}{m}\right)\]
Important
This is the Tsiolkovsky rocket equation. It shows that the change in velocity depends on the exhaust speed (\(u\)) and the ratio of initial to final mass.
When launching from Earth, gravity is an external force \(\vec{F}_{ext} = -mg\hat{j}\).
This adds an impulse \(d\vec{J} = \vec{F}_{ext}dt = -mgdt\hat{j}\).
Including this in momentum conservation: \(mdv - dm_g u = -mgdt\) \(mdv = -dm u - mgdt\) \(dv = -u \frac{dm}{m} - g dt\)
Integrating from \(t=0\) to \(t=\Delta t\) (burn time): \[\Delta v = u \ln\left(\frac{m_0}{m}\right) - g\Delta t\]
Note
The longer the burn time (\(\Delta t\)), the smaller the rocket’s change of velocity will be due to gravity’s opposing force. Rockets need to burn fuel as quickly as possible during liftoff.
| Equation | Description |
|---|---|
| \(\vec{p} = m\vec{v}\) | Linear momentum |
| \(\vec{J} \equiv \int_{t_i}^{t_f}\vec{F}(t)dt\) | Impulse (general) |
| \(\vec{J} = \vec{F}_{ave}\Delta t\) | Impulse (average force) |
| \(\vec{J} = \Delta\vec{p}\) | Impulse-momentum theorem |
| \(\vec{F}_{net} = \frac{d\vec{p}}{dt}\) | Newton’s 2nd Law (momentum form) |
| \(\sum_{j=1}^{N}\vec{p}_j = \text{constant}\) | Conservation of linear momentum |
| Equation | Description |
|---|---|
| \(x_{CM} = \frac{1}{M}\sum m_jx_j\) | X-component of center of mass |
| \(y_{CM} = \frac{1}{M}\sum m_jy_j\) | Y-component of center of mass |
| \(\vec{r}_{CM} = \frac{1}{M}\int\vec{r}dm\) | Center of mass (continuous object) |
| \(\vec{v}_{CM} = \frac{1}{M}\sum m_j\vec{v}_j\) | Velocity of center of mass |
| \(\Delta v = u \ln\left(\frac{m_0}{m}\right)\) | Rocket equation (deep space) |
| \(\Delta v = u \ln\left(\frac{m_0}{m}\right) - g\Delta t\) | Rocket equation (with gravity) |