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Learning Objectives

By the end of this chapter, you should be able to:

Introduction

Chapter 2 replaced the Galilean transformation with the Lorentz transformation, because only the latter is consistent with the invariance of the speed of light. But momentum and energy in Newtonian mechanics are defined and conserved using Galilean kinematics: p=mup = mu, conserved because Newton’s third law and Galilean-invariant forces guarantee it in every Galilean frame. Once the underlying kinematics changes, the old definitions of momentum and energy no longer transform consistently between inertial frames, and a collision that conserves Newtonian momentum in one frame will not, in general, conserve it in another frame related by a Lorentz transformation. This chapter derives the corrected definitions — relativistic momentum and relativistic energy — that are conserved in every inertial frame, assembles them into a single four-component object whose conservation law captures both at once, and works out their most important consequences: mass and energy are, up to a conversion factor c2c^2, the same quantity, and a whole new class of practical calculations — threshold energies for particle production — becomes possible.

3.1Relativistic Momentum

Deriving Relativistic Momentum

Rather than simply asserting the corrected formula, it is worth seeing exactly where it comes from, because the argument is a direct descendant of the light-clock argument used to derive time dilation in Chapter 2, and it makes clear that the correction is forced on us by the Lorentz transformation, not chosen for convenience.

Consider two identical particles, AA and BB, each of rest mass mm, in an idealized elastic scattering event. Choose the incoming and outgoing velocities so that the xx components are unchanged while each particle’s yy component reverses sign. In frame SS, let BB’s transverse speed be w0w_0. Let SS' move at speed vv along the xx-axis relative to SS, and choose SS' so that AA has no xx' motion. In SS', let AA’s transverse speed be the same w0w_0. Because Δy=Δy\Delta y = \Delta y' while Δt=γ(v)(Δt+vΔx/c2)=γ(v)Δt\Delta t = \gamma(v)\left(\Delta t' + v\Delta x'/c^2\right) = \gamma(v)\Delta t' for AA with Δx=0\Delta x' = 0, the transverse speed measured in SS is reduced by a factor of γ(v)\gamma(v):

uy(A)=w0γ(v),as measured in S.u_y(A) = \frac{w_0}{\gamma(v)}, \qquad \text{as measured in } S.

In SS, AA therefore has an xx component vv and a yy component w0/γ(v)-w_0/\gamma(v) before the bounce, while BB has a yy component +w0+w_0. After the bounce, both yy components reverse sign. Writing the momentum of a particle moving at speed uu as p=m(u)up = m(u)\,u, for some as-yet-undetermined function m(u)m(u) that reduces to the particle’s ordinary mass at u=0u=0, conservation of yy momentum says that the incoming and outgoing transverse momenta are equal. Since the outgoing total is the negative of the incoming total, each must be zero; hence

m(u(A))uy(A)    m(u(B))uy(B)  =  0,m\big(u(A)\big)\, |u_y(A)| \;-\; m\big(u(B)\big)\, |u_y(B)| \;=\; 0,

where u(A)u(A) and u(B)u(B) denote the total (not just transverse) speeds of AA and BB in frame SS. Substituting the magnitudes uy(A)=w0/γ(v)|u_y(A)| = w_0/\gamma(v) and uy(B)=w0|u_y(B)| = w_0, and cancelling the common factor of w0w_0,

m(u(A))γ(v)=m(u(B)).\frac{m\big(u(A)\big)}{\gamma(v)} = m\big(u(B)\big).

Finally, take the limit w00w_0 \to 0: in this limit, BB’s transverse motion vanishes entirely, so u(B)0u(B) \to 0 and m(u(B))m(0)mm(u(B)) \to m(0) \equiv m, the particle’s ordinary rest mass. Meanwhile AA’s transverse velocity component also vanishes, leaving AA moving purely along xx at the frame’s relative velocity, so u(A)vu(A) \to v. The boxed relation becomes

m(v)γ(v)=mm(v)=γ(v)m,\frac{m(v)}{\gamma(v)} = m \quad \Longrightarrow \quad m(v) = \gamma(v)\, m,

for arbitrary vv, since vv was the (otherwise unconstrained) relative speed of the two frames. In other words, momentum conservation across inertial frames, together with the Lorentz transformation’s effect on transverse velocities, forces the “effective mass” m(u)m(u) appearing in p=m(u)up = m(u)u to be exactly γ(u)m\gamma(u)m — not simply mm, as Newtonian mechanics assumed. This is the relativistic momentum derived below; unlike the Newtonian formula, it is exactly the definition needed to make momentum conservation frame-independent, consistent with the Lorentz transformation of Chapter 2.

Relativistic Momentum

The result of the argument above is

p=γmu=mu1u2/c2,\vec p = \gamma m \vec u = \frac{m\vec u}{\sqrt{1 - u^2/c^2}},

where mm is the particle’s rest mass — an intrinsic, frame-independent property of the particle, equal to the mass measured by an observer at rest relative to it — and uu is the particle’s speed in the frame in question. For ucu \ll c, γ1\gamma \to 1 and this reduces to the Newtonian p=mu\vec p = m\vec u. As ucu \to c, however, γ\gamma \to \infty, so pp \to \infty as well: a finite force acting for a finite time supplies only a finite impulse, whereas reaching the speed of light would require an unbounded impulse and work. This is the precise dynamical reason no massive object can reach or exceed cc, complementing the kinematic argument of Chapter 2 (relativistic velocity addition never produces ucu \ge c from sub-light inputs).

Worked Example: Testing p=γmup = \gamma m u Against Data

The formula p=γmu\vec p = \gamma m \vec u is not merely a theoretical nicety; it has been tested directly by measuring the momentum and speed of fast electrons and protons independently — momentum from the radius of curvature in a known magnetic field (p=qBrp = qBr), speed from time-of-flight over a measured distance. Measurements of this kind confirm p/(mu)=γ(u)p/(mu) = \gamma(u) across a wide range of speeds and rule out the Newtonian prediction p/(mu)=1p/(mu) = 1 at appreciable fractions of cc. For a proton with u=0.60cu = 0.60c, for instance, γ=1/10.36=1.25\gamma = 1/\sqrt{1-0.36} = 1.25, so the relativistic momentum is 25%25\% larger than the Newtonian formula predicts.

3.2Relativistic Energy

A parallel argument — demanding that the work-energy theorem, dK=FdxdK = \vec F\cdot d\vec x, hold with the relativistic force F=dp/dt\vec F = d\vec p/dt — leads to the relativistic kinetic energy

K=γmc2mc2=(γ1)mc2.K = \gamma mc^2 - mc^2 = (\gamma - 1)mc^2.
Deriving K=(γ1)mc2K = (\gamma-1)mc^2 from the work-energy theorem

Start from the definition of kinetic energy as the work done accelerating a particle from rest to speed uu along a straight line:

K=Fdx=dpdtdx=dpdtudt=udp,K = \int F\,dx = \int \frac{dp}{dt}\,dx = \int \frac{dp}{dt}\,u\,dt = \int u\,dp,

using dx=udtdx = u\,dt. With p=γmu=mu/1u2/c2p = \gamma m u = mu/\sqrt{1-u^2/c^2}, differentiating with respect to uu gives

dpdu=m[11u2/c2+u2/c2(1u2/c2)3/2]=m(1u2/c2)3/2=γ3m,\frac{dp}{du} = m\left[\frac{1}{\sqrt{1-u^2/c^2}} + \frac{u^2/c^2}{(1-u^2/c^2)^{3/2}}\right] = \frac{m}{(1-u^2/c^2)^{3/2}} = \gamma^3 m,

so dp=γ3mdudp = \gamma^3 m\,du, and

K=0uuγ3(u)mdu=m0uudu(1u2/c2)3/2.K = \int_0^u u'\,\gamma^3(u') m\,du' = m\int_0^u \frac{u'\,du'}{(1-u'^2/c^2)^{3/2}}.

Substituting s=1u2/c2s = 1 - u'^2/c^2, ds=2udu/c2ds = -2u'\,du'/c^2, the integral becomes elementary:

K=mc211u2/c2(12)s3/2ds=mc2[s1/2]11u2/c2=mc2(11u2/c21),K = mc^2\int_{1}^{1-u^2/c^2} \left(-\tfrac12\right)s^{-3/2}\,ds = mc^2\Big[s^{-1/2}\Big]_{1}^{1-u^2/c^2} = mc^2\left(\frac{1}{\sqrt{1-u^2/c^2}} - 1\right),

which is exactly K=(γ1)mc2K = (\gamma - 1)mc^2 — confirming, by direct integration of the relativistic work-energy theorem, the result quoted in the main text.

It is useful to expand this for ucu \ll c using the binomial approximation γ1+12u2/c2+\gamma \approx 1 + \tfrac{1}{2}u^2/c^2 + \cdots:

K(1+12u2c2)mc2mc2=12mu2,K \approx \left(1 + \frac{1}{2}\frac{u^2}{c^2}\right)mc^2 - mc^2 = \frac{1}{2}mu^2,

recovering the familiar Newtonian kinetic energy as the low-speed limit — a necessary consistency check, since Newtonian mechanics is extremely well tested at everyday speeds.

The kinetic energy expression separates naturally into two terms: γmc2\gamma mc^2, and a constant mc2mc^2 subtracted off. Einstein’s insight was to take both terms seriously as energy, not just their difference. Define the total energy

E=γmc2,E = \gamma mc^2,

and the rest energy

E0=mc2.E_0 = mc^2.

Then K=EE0K = E - E_0: kinetic energy is the energy above and beyond the energy mc2mc^2 a particle possesses simply by virtue of having rest mass mm, even at rest (u=0u=0, γ=1\gamma=1). This is the celebrated mass–energy equivalence: rest mass is a form of energy, convertible (in principle and, in nuclear and particle processes, routinely in practice) into other forms of energy, and vice versa. The conversion factor c29×1016 m2/s2c^2 \approx 9\times 10^{16}\ \text{m}^2/\text{s}^2 is enormous, which is why converting even a small amount of rest mass releases a very large amount of energy — the physical basis of the energy released in nuclear fission and fusion, examined in Chapter 13.

3.3Four-Vectors and Threshold Energies

The Energy–Momentum Four-Vector

Momentum and energy are not independent; eliminating uu and γ\gamma between p=γmu\vec p = \gamma m\vec u and E=γmc2E = \gamma mc^2 gives the energy–momentum invariant,

E2=(pc)2+(mc2)2,E^2 = (pc)^2 + (mc^2)^2,

a relation that holds for every particle, in every inertial frame.

This is directly analogous to the invariant spacetime interval (Δs)2=c2Δt2Δx2(\Delta s)^2 = c^2\Delta t^2 - \Delta x^2 of Chapter 2, and the analogy is not superficial: just as (ct,x,y,z)(ct, x, y, z) can be assembled into a single spacetime-displacement four-vector that transforms under a Lorentz boost according to the Lorentz transformation, the quadruple (E/c,px,py,pz)(E/c, p_x, p_y, p_z) can be assembled into a single energy–momentum four-vector,

pμ=(Ec,px,py,pz),p^\mu = \left(\frac{E}{c},\, p_x,\, p_y,\, p_z\right),

which transforms from one inertial frame to another by exactly the same Lorentz transformation rule used for (ct,x,y,z)(ct,x,y,z) in Chapter 2 (with ctE/cct \to E/c and xpxx \to p_x). Its invariant magnitude is

(Ec)2px2py2pz2=(mc)2,\left(\frac{E}{c}\right)^2 - p_x^2 - p_y^2 - p_z^2 = (mc)^2,

which is precisely the energy–momentum relation in Equation (3.14), rearranged; the rest mass mm plays the same role for the energy–momentum four-vector that the invariant interval plays for the spacetime-displacement four-vector — a quantity every observer computes to be the same, regardless of the frame in which EE and p\vec p individually are measured. For a massive particle, the energy–momentum four-vector is proportional to its four-velocity. Its component ratio therefore gives the ordinary velocity, vx=pxc2/Ev_x = p_xc^2/E (and similarly for the other components). A slower particle has a larger ratio of E/cE/c to its momentum, as this expression requires.

The relation can be read geometrically as a right triangle, as shown in Figure 3.1: the total-energy term is the hypotenuse, while rest energy and momentum provide the two legs.

Right-triangle diagram showing total energy E as the hypotenuse and mc squared and pc as the legs.

Figure 3.1:The energy–momentum relation as a right triangle: E2=(pc)2+(mc2)2E^2=(pc)^2+(mc^2)^2. Original schematic by the author.

Two limits of the energy–momentum relation are worth committing to memory:

The energy–momentum relation is often more convenient than working with uu and γ\gamma directly, particularly for high-energy particles and for photons, where speed is fixed at cc and carries no information about energy.

Why the Four-Vector Formalism Earns Its Keep

The payoff of packaging (E/c,p)(E/c, \vec p) as a single object is that the energy–momentum four-vector is exactly conserved in every collision or decay, in every inertial frame, component by component — precisely because the underlying, separately-conserved quantities (in every frame) are energy and the three components of momentum. This means a conservation calculation can be carried out entirely by four-vector addition: add up the four-vectors of everything going into a collision, add up the four-vectors of everything coming out, and set the two sums equal, four components at a time. Because the four-vector’s magnitude, (E/c)2p2=(mc)2(E/c)^2 - p^2 = (mc)^2, is invariant, this magnitude can be computed in whichever frame is most convenient — often a frame in which one particle is initially at rest, or the frame in which the total three-momentum is zero (the subject of the next section) — and the resulting relation between energies and masses will hold in every other frame as well.

Electron–positron annihilation, revisited: consider an electron and a positron (each of mass mm), both essentially at rest, annihilating. Charge conservation alone would permit e+e+γe^- + e^+ \to \gamma (a single photon), but the four-vector of the initial state is (2mc,0,0,0)(2mc, 0,0,0) (both particles at rest, energies mc2mc^2 each, zero total momentum), while any single photon’s four-vector must satisfy E=pcE=pc, i.e., have equal, nonzero energy and momentum magnitude — it cannot have zero momentum unless its energy is also zero. A single outgoing photon is therefore impossible; conservation of the energy–momentum four-vector, not merely of energy or momentum separately, forces at least two photons, emitted back-to-back so that their momenta cancel, each carrying energy mc2mc^2. This is the same conclusion reached by separate energy and momentum arguments in Problem 3 below, but the four-vector language makes clear that both conservation laws are really a single, unified statement, and this is exactly the physical process (positron annihilation, producing two back-to-back 511 keV511\ \text{keV} gamma rays) exploited in medical positron-emission tomography (PET) scans to locate a radioactive tracer inside the body.

Center-of-Momentum Frame and Threshold Energies

Many practical problems in nuclear and particle physics — will one particle collision produce a new particle, or not? — are most easily solved by transforming to the center-of-momentum (CM) frame: the unique inertial frame in which the total three-momentum of a system is zero. Because (E/c)2p2(E/c)^2 - p^2 is Lorentz-invariant, the total invariant mass of a system of particles,

(Mc2)2Etotal2(ptotalc)2,(Mc^2)^2 \equiv E_{\text{total}}^2 - (p_{\text{total}}c)^2,

is the same number whether computed in the lab frame or in the CM frame — but in the CM frame, where ptotal=0p_{\text{total}} = 0 by definition, it simplifies to Mc2=Etotal,CMMc^2 = E_{\text{total,CM}}: the total CM-frame energy alone. This invariant MM determines whether a reaction is kinematically possible: by conservation of the energy-momentum four-vector, a reaction that produces a set of final-state particles with total rest mass mf\sum m_f is only possible if the available energy in the CM frame is at least (mf)c2\left(\sum m_f\right)c^2 — i.e., if MmfM \ge \sum m_f. Other conservation laws and interaction probabilities can still forbid or suppress a reaction. The threshold condition is M=mfM = \sum m_f exactly, corresponding, for massive final-state particles, to all of them being at rest relative to the CM frame (and hence relative to each other), with no leftover kinetic energy to spare.

The CM frame is not a relativistic invention, and it is worth recovering the non-relativistic intuition before leaning on it. Figure 3.2 runs elastic and inelastic collisions in one and two dimensions, with the center of mass drawn on the screen and a momentum diagram beside it. Whatever the pucks do, that marker glides on at constant velocity — the collision cannot touch it, because the internal forces cancel in pairs — which is what makes its rest frame a natural place to do the bookkeeping. Choose the masses and velocities so that the marker stands still, and the momentum diagram shows what has been bought: two arrows equal and opposite before the collision, two arrows equal and opposite after it, however much kinetic energy was lost in between. The relativistic version below keeps that structure exactly, replacing mum\vec u by γmu\gamma m \vec u and the total mass by the invariant MM; what changes is that MM is no longer the sum of the parts.

Screenshot of the Collision Lab simulation

Figure 3.2:Classical collisions with the center of mass and the momentum vectors displayed. The center of mass moves at a velocity no collision can change, elastic or not, which is what makes its rest frame a natural place to do the bookkeeping — and what carries over, with γmu\gamma m\vec u in place of mum\vec u, to the relativistic threshold calculations of this section.

Interactive simulation: Collision Lab

Worked Example: The Threshold for Antiproton Production

In 1955, the Bevatron at Berkeley was built specifically to search for the antiproton, via the reaction

p+pp+p+p+pˉ,p + p \to p + p + p + \bar p,

a proton beam striking a stationary proton (in a hydrogen target), producing an additional proton–antiproton pair. (Baryon number and charge are each automatically conserved by this reaction; nothing prevents it kinematically once enough energy is available.) What is the minimum, or threshold, kinetic energy the beam proton must have, in the lab frame, where the target proton is at rest?

Let mm be the proton (and antiproton) rest mass, m1=m2=mm_1 = m_2 = m for beam and target, and let M=4mM = 4m be the total rest mass of the four final-state particles, all momentarily at rest in the CM frame at threshold. The invariant M2c4=Etotal2(ptotalc)2M^2c^4 = E_{\text{total}}^2 - (p_{\text{total}}c)^2 can be computed in the lab frame, where the target is at rest (E2=mc2E_2 = mc^2, p2=0p_2 = 0) and the beam proton has energy E1E_1 and momentum p1p_1:

(4mc2)2=(E1+mc2)2(p1c)2=E12+2E1mc2+m2c4(p1c)2.(4mc^2)^2 = (E_1 + mc^2)^2 - (p_1c)^2 = E_1^2 + 2E_1mc^2 + m^2c^4 - (p_1c)^2.

Using E12(p1c)2=(mc2)2E_1^2 - (p_1c)^2 = (mc^2)^2 (the beam proton’s own invariant), this simplifies to

16m2c4=m2c4+2E1mc2+m2c4E1=7mc2.16m^2c^4 = m^2c^4 + 2E_1mc^2 + m^2c^4 \quad \Longrightarrow \quad E_1 = 7mc^2.

The threshold kinetic energy is K1=E1mc2=6mc2K_1 = E_1 - mc^2 = 6mc^2. With mc2=938 MeVmc^2 = 938\ \text{MeV} for the proton, this is K1=6(938 MeV)=5.6 GeVK_1 = 6(938\ \text{MeV}) = 5.6\ \text{GeV} — dramatically larger than the naive 2mc2=2(938 MeV)=1.9 GeV2mc^2 = 2(938\ \text{MeV}) = 1.9\ \text{GeV} one might have guessed from simply counting the rest-mass energy of the new particle pair. The extra factor of three arises because, in the lab frame, the newly created particles must all share the same velocity as the CM frame itself (since at threshold they are at rest in the CM frame, which is itself moving relative to the lab), so a substantial fraction of the beam’s kinetic energy is unavoidably “wasted” maintaining the overall forward motion of the collision products rather than being converted into new rest mass. The Bevatron was deliberately designed to reach a beam energy of 6.2 GeV6.2\ \text{GeV}, comfortably above this threshold, and the antiproton was discovered there later that same year by Owen Chamberlain, Emilio Segrè, and collaborators.

This “wasted energy” problem is exactly why modern particle physics favors colliders, in which two beams travel toward each other and collide head-on. If the beam and target in the reaction above were replaced by two protons of equal and opposite momentum (so that the lab frame is the CM frame), the threshold condition becomes simply 2E1=4mc22E_1 = 4mc^2, i.e., K1=mc2K_1 = mc^2 per beam — six times less kinetic energy required per proton than the fixed-target case, precisely because no energy needs to be spent maintaining a net forward CM velocity.

The contrast between the two arrangements is summarized in Figure 3.3.

Comparison of a fixed-target collision, which retains forward momentum, and a head-on collider collision, whose total momentum is zero.

Figure 3.3:Fixed-target versus collider kinematics. In a head-on collider the center-of-momentum frame can coincide with the laboratory, so more of the beam energy is available to create rest mass. Original schematic by the author.

The historical setting of this threshold calculation is shown in Figure 3.4: the Bevatron was built in the 1950s to reach the energies needed to discover the antiproton.

Historical photograph of the interior of the Bevatron accelerator building at Lawrence Berkeley National Laboratory.

Figure 3.4:Interior of the former Bevatron building at Lawrence Berkeley National Laboratory. Photograph by Daniel Parks, 2010; CC BY 2.0 via Wikimedia Commons. The photograph shows the surviving facility structure, not the operating 1955 machine.

Aside: Why There Are No Faster-Than-Light Massive Particles

Chapter 2 argued, from causality alone, that no signal or influence can travel faster than cc without permitting effects to precede their causes in some valid inertial frame. This chapter’s momentum formula, p=γmup = \gamma m u, gives an independent, purely dynamical reason a massive particle in particular can never reach or exceed cc: as ucu \to c^-, γ\gamma \to \infty, so accelerating a massive particle arbitrarily close to cc requires arbitrarily large — and, at u=cu=c itself, literally infinite — momentum and energy. No finite amount of work can supply this, so cc is a strict, unreachable asymptote for any object with m>0m>0, approached but never attained no matter how long or how powerfully it is accelerated.

It is sometimes asked whether a hypothetical particle might simply be born moving faster than cc, without ever having to accelerate through cc — such a hypothetical particle is called a tachyon. Formally, applying the energy–momentum relation at u>cu>c gives a spacelike four-momentum, so the invariant mass-squared would be negative (often described informally as an “imaginary rest mass”). This is not the rest mass of an ordinary particle, and no such particle has been observed. More importantly, a tachyon would connect spacelike-separated events (Chapter 2) — and the causality argument there shows that some inertial observer would measure any spacelike-connecting signal to travel backward in time, arriving before it was sent. Thus the mass–energy relation excludes faster-than-light motion for ordinary massive particles, while the light-cone argument gives a separate causal reason that controllable faster-than-light signals cannot exist.

Worked Example: An Electron Accelerated Through a Potential Difference

An electron (rest energy mc2=0.511 MeVm c^2 = 0.511\ \text{MeV}) is accelerated from rest through a potential difference of 2.00 MV2.00\ \text{MV}, gaining kinetic energy K=qV=2.00 MeVK = qV = 2.00\ \text{MeV}.

Total energy: E=K+mc2=2.00 MeV+0.511 MeV=2.511 MeVE = K + mc^2 = 2.00\ \text{MeV} + 0.511\ \text{MeV} = 2.511\ \text{MeV}.

Momentum: from E2=(pc)2+(mc2)2E^2 = (pc)^2 + (mc^2)^2,

pc=E2(mc2)2=(2.511 MeV)2(0.511 MeV)2=2.458 MeV,pc = \sqrt{E^2 - (mc^2)^2} = \sqrt{(2.511\ \text{MeV})^2 - (0.511\ \text{MeV})^2} = 2.458\ \text{MeV},

so p=2.458 MeV/cp = 2.458\ \text{MeV}/c.

Speed: from E=γmc2E = \gamma mc^2, γ=E/mc2=(2.511 MeV)/(0.511 MeV)=4.914\gamma = E/mc^2 = (2.511\ \text{MeV})/(0.511\ \text{MeV}) = 4.914, and u=c11/γ2=0.979cu = c\sqrt{1 - 1/\gamma^2} = 0.979c.

Note that a Newtonian calculation of the speed from K=12mu2K = \tfrac12 mu^2 would give u=c2K/mc2=c2(2.00 MeV)/(0.511 MeV)2.8cu = c\sqrt{2K/mc^2} = c\sqrt{2(2.00\ \text{MeV})/(0.511\ \text{MeV})} \approx 2.8c — an unphysical result exceeding cc, and a sharp reminder that the Newtonian kinetic-energy formula must not be used once KK is comparable to or larger than mc2mc^2.

3.4Summary

3.5Problems

Solution to Exercise 3.1 #

The Lorentz factor is

γ=11(0.900)2=2.294.\gamma=\frac{1}{\sqrt{1-(0.900)^2}}=2.294.

The total energy is

E=γmc2=(2.294)(938 MeV)=2.15×103 MeV.E=\gamma mc^2=(2.294)(938\ \text{MeV})=2.15\times10^3\ \text{MeV}.

The kinetic energy is

K=Emc2=(2.15×103 MeV)(938 MeV)=1.21×103 MeV.K=E-mc^2=(2.15\times10^3\ \text{MeV})-(938\ \text{MeV}) =1.21\times10^3\ \text{MeV}.

Finally,

p=γmu=γucmc2c=(2.294)(0.900)938 MeVc=1.94×103 MeV/c.p=\gamma m u=\gamma\frac{u}{c}\frac{mc^2}{c} =(2.294)(0.900)\frac{938\ \text{MeV}}{c} =1.94\times10^3\ \text{MeV}/c.

Therefore, the proton has γ=2.294\gamma=2.294, E=2.15×103 MeVE=2.15\times10^3\ \text{MeV}, K=1.21×103 MeVK=1.21\times10^3\ \text{MeV}, and p=1.94×103 MeV/cp=1.94\times10^3\ \text{MeV}/c.

Solution to Exercise 3.2 #

Write β=u/c\beta=u/c. The ratio is

KrelKNewt=(γ1)mc212mβ2c2=2(γ1)β2.\frac{K_\mathrm{rel}}{K_\mathrm{Newt}} =\frac{(\gamma-1)mc^2}{\tfrac12 m\beta^2c^2} =\frac{2(\gamma-1)}{\beta^2}.

For a 10%10\% difference, set this ratio equal to 1.10. Since β2=11/γ2\beta^2=1-1/\gamma^2,

2(γ1)11/γ2=1.102γ2γ+1=1.10.\frac{2(\gamma-1)}{1-1/\gamma^2}=1.10 \quad\Longrightarrow\quad \frac{2\gamma^2}{\gamma+1}=1.10.

Thus

2γ21.10γ1.10=0,γ=1.06597,2\gamma^2-1.10\gamma-1.10=0, \qquad \gamma=1.06597,

where the positive root was chosen. Hence

β=11γ2=0.346.\beta=\sqrt{1-\frac{1}{\gamma^2}} =0.346.

Therefore, the relativistic kinetic energy is 10%10\% larger than the Newtonian prediction at u0.346c=1.04×108 m/su\approx0.346c=1.04\times10^8\ \text{m/s}.

Solution to Exercise 3.3 #

Initially, both particles are essentially at rest, so their total energy is their combined rest energy:

Ei=(0.511 MeV)+(0.511 MeV)=1.022 MeV.E_i=(0.511\ \text{MeV})+(0.511\ \text{MeV})=1.022\ \text{MeV}.

If the two photons have equal energy EγE_\gamma, energy conservation gives

2Eγ=1.022 MeV,Eγ=0.511 MeV.2E_\gamma=1.022\ \text{MeV}, \qquad E_\gamma=0.511\ \text{MeV}.

The initial total momentum is zero. Each photon has momentum magnitude pγ=Eγ/cp_\gamma=E_\gamma/c, so two equal nonzero momentum vectors can sum to zero only if they point in opposite directions. Therefore, the annihilation produces two photons of energy 0.511 MeV0.511\ \text{MeV} each, traveling in exactly opposite directions.

Diagrams of electron-positron annihilation and pion decay showing two products travelling in opposite directions.

Figure 3.5:For any two-body process whose parent is at rest, momentum conservation fixes the products to have equal and opposite momenta. The right panel also previews the geometry used in the next solution.

Solution to Exercise 3.4 #

The pion is initially at rest, so its total momentum is zero. The muon and massless neutrino must therefore have equal and opposite momentum magnitude pp. Their energies are

Eμ=(pc)2+(105.7 MeV)2,Eν=pc.E_\mu=\sqrt{(pc)^2+(105.7\ \text{MeV})^2}, \qquad E_\nu=pc.

Energy conservation gives

139.6 MeV=Eμ+pc.139.6\ \text{MeV}=E_\mu+pc.

Substitute pc=139.6 MeVEμpc=139.6\ \text{MeV}-E_\mu into the muon’s energy relation:

Eμ2=(139.6 MeVEμ)2+(105.7 MeV)2.E_\mu^2=(139.6\ \text{MeV}-E_\mu)^2+(105.7\ \text{MeV})^2.

Expanding and cancelling Eμ2E_\mu^2 yields

2(139.6 MeV)Eμ=(139.6 MeV)2+(105.7 MeV)2,2(139.6\ \text{MeV})E_\mu=(139.6\ \text{MeV})^2+(105.7\ \text{MeV})^2,

so

Eμ=(139.6 MeV)2+(105.7 MeV)22(139.6 MeV)=109.8 MeV.E_\mu=\frac{(139.6\ \text{MeV})^2+(105.7\ \text{MeV})^2}{2(139.6\ \text{MeV})} =109.8\ \text{MeV}.

Therefore, the muon’s kinetic energy is Kμ=109.8 MeV105.7 MeV=4.1 MeVK_\mu=109.8\ \text{MeV}-105.7\ \text{MeV}=4.1\ \text{MeV}.

The pion-decay panel in Figure 3.5 shows why the muon and neutrino use the same momentum magnitude pp in the energy calculation.

Solution to Exercise 3.5 #

Starting with the definitions,

E2=(γmc2)2=γ2m2c4E^2=(\gamma mc^2)^2=\gamma^2m^2c^4

and

(pc)2=(γmuc)2=γ2m2u2c2.(pc)^2=(\gamma mu c)^2=\gamma^2m^2u^2c^2.

Subtracting gives

E2(pc)2=γ2m2c4γ2m2u2c2=γ2m2c4(1u2c2)=m2c4,\begin{aligned} E^2-(pc)^2 &=\gamma^2m^2c^4-\gamma^2m^2u^2c^2\\ &=\gamma^2m^2c^4\left(1-\frac{u^2}{c^2}\right)\\ &=m^2c^4, \end{aligned}

because γ2(1u2/c2)=1\gamma^2(1-u^2/c^2)=1. Therefore, rearranging gives E2=(pc)2+(mc2)2E^2=(pc)^2+(mc^2)^2.

Solution to Exercise 3.6 #

Mass--energy equivalence gives P=(Δm/Δt)c2P=(\Delta m/\Delta t)c^2, so

ΔmΔt=Pc2=3.8×1026 J/s(3.00×108 m/s)2=4.2×109 kg/s.\frac{\Delta m}{\Delta t}=\frac{P}{c^2} =\frac{3.8\times10^{26}\ \text{J/s}}{(3.00\times10^8\ \text{m/s})^2} =4.2\times10^9\ \text{kg/s}.

The elapsed time is

t=(4.6×109 yr)(3.156×107 s/yr)=1.45×1017 s.t=(4.6\times10^9\ \text{yr})\left(3.156\times10^7\ \text{s/yr}\right) =1.45\times10^{17}\ \text{s}.

At the stated constant rate, the lost mass would be

Δm=(4.2×109 kg/s)(1.45×1017 s)=6.1×1026 kg.\Delta m=(4.2\times10^9\ \text{kg/s})(1.45\times10^{17}\ \text{s}) =6.1\times10^{26}\ \text{kg}.

Its fraction of the Sun’s mass is

ΔmM=6.1×1026 kg2.0×1030 kg=3.1×104=0.031%.\frac{\Delta m}{M_\odot}=\frac{6.1\times10^{26}\ \text{kg}}{2.0\times10^{30}\ \text{kg}} =3.1\times10^{-4}=0.031\%.

Therefore, the Sun loses about 4.2×109 kg4.2\times10^9\ \text{kg} each second to radiation, but this amounts to only about 0.031%0.031\% of its present mass over 4.6 billion years and is not significant for its lifetime so far.

Solution to Exercise 3.7 #

Substitution of uy(A)=w0/γ(v)u_y(A)=w_0/\gamma(v) into transverse-momentum conservation gives

m(u(A))w0γ(v)=m(u(B))w0.m(u(A))\frac{w_0}{\gamma(v)}=m(u(B))w_0.

For nonzero w0w_0, cancel w0w_0:

m(u(A))γ(v)=m(u(B)).\frac{m(u(A))}{\gamma(v)}=m(u(B)).

As w00w_0\to0, particle BB has only its vanishing transverse motion, so u(B)0u(B)\to0 and m(u(B))m(0)=mm(u(B))\to m(0)=m. Particle AA has ux(A)=vu_x(A)=v and uy(A)=w0/γ(v)0u_y(A)=w_0/\gamma(v)\to0, so

u(A)=v2+[w0γ(v)]2v.u(A)=\sqrt{v^2+\left[\frac{w_0}{\gamma(v)}\right]^2}\longrightarrow v.

Consequently,

m(v)γ(v)=m,m(v)=γ(v)m.\frac{m(v)}{\gamma(v)}=m, \qquad m(v)=\gamma(v)m.

Therefore, the momentum law required by this limiting collision argument is p=γmu\vec p=\gamma m\vec u.

Solution to Exercise 3.8 #

For u=0.60cu=0.60c,

γ=11(0.60)2=1.25.\gamma=\frac{1}{\sqrt{1-(0.60)^2}}=1.25.

Each lump has energy E=γmc2=1.25mc2E=\gamma mc^2=1.25mc^2. Their momenta are equal and opposite, so the total initial four-vector is

(Etotc,ptot)=(2(1.25mc2)c,0)=(2.50mc2c,0).\left(\frac{E_\mathrm{tot}}{c},p_\mathrm{tot}\right) =\left(\frac{2(1.25mc^2)}{c},0\right) =\left(\frac{2.50mc^2}{c},0\right).

The composite is at rest, so its four-vector is (Mc,0)(Mc,0); conservation gives

Mc2=2.50mc2,M=2.50m.Mc^2=2.50mc^2, \qquad M=2.50m.

Therefore, the stuck-together lump has rest mass 2.50m2.50m, not 2m2m; the extra 0.50mc20.50mc^2 is the original kinetic energy retained as internal energy, such as heat and deformation, in the composite.

Solution to Exercise 3.9 #

At threshold, the final particles are at rest relative to one another in the CM frame, so their total rest mass is

M=2mp+mX=2mp+10mp=12mp.M=2m_p+m_X=2m_p+10m_p=12m_p.

For a stationary target, the initial invariant is

M2c4=(Eb+mpc2)2(pbc)2=2mp2c4+2Ebmpc2,M^2c^4=(E_b+m_pc^2)^2-(p_bc)^2 =2m_p^2c^4+2E_bm_pc^2,

where Eb2(pbc)2=mp2c4E_b^2-(p_bc)^2=m_p^2c^4 was used. Set this equal to (12mpc2)2(12m_pc^2)^2:

144mp2c4=2mp2c4+2Ebmpc2,144m_p^2c^4=2m_p^2c^4+2E_bm_pc^2,

so

Eb=71mpc2,Kb=Ebmpc2=70mpc2.E_b=71m_pc^2, \qquad K_b=E_b-m_pc^2=70m_pc^2.

For equal and opposite collider beams, the lab is the CM frame, and threshold requires

2Eb=12mpc2,Eb=6mpc2,Kb=5mpc22E_b=12m_pc^2, \qquad E_b=6m_pc^2, \qquad K_b=5m_pc^2

per proton. The ratio is

70mpc25mpc2=14.\frac{70m_pc^2}{5m_pc^2}=14.

Therefore, the fixed-target threshold is 70mpc270m_pc^2 of kinetic energy, the collider threshold is 5mpc25m_pc^2 per beam proton, and colliders require fourteen times less kinetic energy per incident proton because the CM has no net forward motion.

Comparison of a fixed-target collision with a head-on collider collision, showing centre-of-momentum motion only in the fixed-target case.

Figure 3.6:In a fixed-target experiment, much of the beam energy remains as forward centre-of-momentum motion; in a collider, that energy is available to create new rest mass.

Solution to Exercise 3.10 #

The initial photon and electron have total momentum pγ=Eγ/cp_\gamma=E_\gamma/c in the photon direction, so the final particle must recoil with that momentum. The invariant mass of the one-particle final state follows from the initial four-vector:

M2c4=(mc2+Eγ)2(pγc)2=(mc2+Eγ)2Eγ2=m2c4+2mc2Eγ.\begin{aligned} M^2c^4&=(mc^2+E_\gamma)^2-(p_\gamma c)^2\\ &=(mc^2+E_\gamma)^2-E_\gamma^2\\ &=m^2c^4+2mc^2E_\gamma. \end{aligned}

Thus

M=m2+2mEγc2.M=\sqrt{m^2+\frac{2mE_\gamma}{c^2}}.

Therefore, the final particle has momentum p=Eγ/cp=E_\gamma/c and rest mass M=m2+2mEγ/c2M=\sqrt{m^2+2mE_\gamma/c^2}. Its total energy is mc2+Eγmc^2+E_\gamma, as required by energy conservation.

Solution to Exercise 3.11 #

For a particle with finite nonzero energy, p=Eu/c2p=Eu/c^2, so the invariant becomes

m2c4=E2(pc)2=E2(Euc)2=E2(1u2c2).m^2c^4=E^2-(pc)^2 =E^2-\left(\frac{Eu}{c}\right)^2 =E^2\left(1-\frac{u^2}{c^2}\right).

At u=1.5cu=1.5c,

m2c4=E2(12.25)=1.25E2<0,m^2c^4=E^2(1-2.25)=-1.25E^2<0,

so m2<0m^2<0. Such a signal connects spacelike-separated events. For a spacelike separation, a Lorentz transformation can reverse the order of emission and reception, so some inertial observer would see the signal arrive before it was sent; combining such signals between suitably moving observers permits a reply to reach the sender before the original message. Therefore, a tachyon requires negative mass squared in this formalism and would permit a causality paradox even apart from that problem.

Solution to Exercise 3.12 #

At threshold the incident proton has Eb=7mc2E_b=7mc^2 and the stationary target has energy mc2mc^2, so

Etot=8mc2.E_\mathrm{tot}=8mc^2.

The beam momentum follows from its invariant:

pbc=Eb2m2c4=(7mc2)2(mc2)2=48mc2=43mc2.p_bc=\sqrt{E_b^2-m^2c^4} =\sqrt{(7mc^2)^2-(mc^2)^2} =\sqrt{48}\,mc^2=4\sqrt3\,mc^2.

The CM frame moves at V=c2ptot/EtotV=c^2p_\mathrm{tot}/E_\mathrm{tot}, hence

V=c2(43mc)8mc2=32c=0.866c.V=\frac{c^2(4\sqrt3\,mc)}{8mc^2} =\frac{\sqrt3}{2}c =0.866c.

The final four-particle system has rest energy 4mc24mc^2 but lab energy 8mc28mc^2; its Lorentz factor in the lab is γCM=8mc2/(4mc2)=2\gamma_\mathrm{CM}=8mc^2/(4mc^2)=2, consistent with V=0.866cV=0.866c. Therefore, the naive 2mc22mc^2 counts only the new pair’s rest energy, whereas the additional 4mc24mc^2 of the 6mc26mc^2 beam kinetic energy is unavoidable kinetic energy of the entire final system moving at 0.866c0.866c in the lab.

The fixed-target panel of Figure 3.6 illustrates this forward-moving final centre of mass.