Special Relativity — worked problems
4-velocities and $\gamma$ as an inner product
(a) In an inertial frame $S$ an object has 3-velocity $\vec u$. A frame $S'$ moves in the negative $x$-direction relative to $S$ with relative speed $v'$. Write down the 4-velocities of the object and of $S'$ in $S$. (b) Show that $\gamma$ of an object in any frame equals the inner product of its 4-velocity with the 4-velocity of an observer at rest in that frame. (c) Express the $\gamma$ factor of the object in (a) in frame $S'$.
(a) The two 4-velocities in $S$
The 4-velocity of a particle is $U^\mu = dx^\mu/d\tau = \gamma(c, \vec u)$ where $\gamma = (1-u^2/c^2)^{-1/2}$. Applying this to the object,
$$U^\mu = \gamma_u(c,\,\vec u),\qquad \gamma_u = (1 - u^2/c^2)^{-1/2}.$$
The frame $S'$ moves at $-v'\hat x$ relative to $S$. An observer at rest in $S'$ has 3-velocity $-v'\hat x$ in $S$, so
$$V^\mu = \gamma_{v'}(c,\,-v',0,0),\qquad \gamma_{v'} = (1 - v'^2/c^2)^{-1/2}.$$
(b) $\gamma$ from the inner product
Evaluate $U\!\cdot\!V = U^\mu V_\mu = U^0 V^0 - \vec U\!\cdot\!\vec V$ in the rest frame $\tilde S$ of the observer, where $\tilde V^\mu = (c,\vec 0)$ and the object has 4-velocity $\tilde U^\mu = \gamma_{\tilde u}(c,\vec{\tilde u})$:
$$U\!\cdot\!V = \gamma_{\tilde u}\,c^2 - 0 = \gamma_{\tilde u}\,c^2.$$
$U\!\cdot\!V$ is a Lorentz scalar — the same number in every frame. So in any frame,
$$\boxed{\;\gamma_{\tilde u} = \frac{U\!\cdot\!V}{c^2}.\;}$$
(c) Apply to frame $S'$
Compute $U\!\cdot\!V$ in $S$ using the components above:
$$U\!\cdot\!V = \gamma_u\gamma_{v'}\bigl[c\cdot c - \vec u\!\cdot\!(-v'\hat x)\bigr] = \gamma_u\gamma_{v'}(c^2 + u_x v').$$
Dividing by $c^2$,
$$\boxed{\;\gamma_{u'} = \gamma_u\gamma_{v'}\!\left(1+\frac{u_x v'}{c^2}\right).\;}$$
Sanity checks
- $\vec u = 0$: object at rest in $S$ ⇒ in $S'$ it moves at $-v'\hat x$, giving $\gamma_{u'} = \gamma_{v'}$. ✓
- $\vec u = -v'\hat x$: object is at rest in $S'$, so $\gamma_{u'} = 1$; formula gives $\gamma_u\gamma_{v'}(1 - v'^2/c^2) = \gamma_{v'}/\gamma_{v'} \cdot 1 = 1$. ✓
A single Lorentz-invariant contraction $U\!\cdot\!V$ encodes the full relativistic velocity-addition algebra, cross-referenced with Problem 1.3.
Light signal and rescue ship
You are traveling at relative speed $c/4$ toward a space station; when you send a light signal for help, the distance to the station in your frame is 1 light-day. The station dispatches a rescue ship at speed $3c/4$ relative to itself. How long, on your clock, does (a) the light signal take to reach the station, and (b) the rescue ship to reach you?
Setup
Work entirely in your rest frame to avoid juggling proper-time corrections (you measure both intervals on your single clock). Place yourself at $x = 0$. The station approaches you at $-c/4$; in your frame its current distance is $L_0 = 1$ light-day.
Phase 1: light signal reaches the station
Light leaves at $t = 0$ from $x = 0$ moving at $+c$. The station's position is $x_\text{stn}(t) = L_0 - (c/4)t$. Intersection:
$$ct_1 = L_0 - \tfrac{c}{4}t_1 \;\Longrightarrow\; t_1 = \frac{4 L_0}{5c} = 0.8\text{ day.}$$
Station location at reception: $x_1 = c t_1 = 4L_0/5 = 0.8$ ly.
Phase 2: rescue-ship velocity in your frame
The ship leaves the station at speed $3c/4$ "relative to itself" — i.e. relative to the station, in the station's frame. The station has lab velocity $-c/4$ and the ship moves at $-3c/4$ in the station frame (toward you, i.e. in the $-\hat x$ direction). Relativistic velocity addition:
$$u_\text{res} = \frac{-3c/4 - c/4}{1 + (3c/4)(c/4)/c^2} = \frac{-c}{1 + 3/16} = -\frac{16}{19}c.$$
Phase 3: rescue-ship travel time
Ship starts from $x_1 = 4L_0/5$, moves at $|u_\text{res}| = 16c/19$ toward $x = 0$:
$$\Delta t_2 = \frac{x_1}{|u_\text{res}|} = \frac{4L_0/5}{16c/19} = \frac{19 L_0}{20 c} = 0.95\text{ day.}$$
Total time on your clock
$$\boxed{\;t_\text{total} = t_1 + \Delta t_2 = \frac{4L_0}{5c} + \frac{19L_0}{20c} = \frac{7 L_0}{4c} = 1.75\text{ day} = 42\text{ h.}\;}$$
Newtonian shortcut would have given $u_\text{res}^\text{Newt} = -c$, conflicting with light-speed limit; the relativistic answer differs by ~16% — significant for any space-rescue scheduler.
Relativistic pursuit at constant proper acceleration
A police officer at rest in $S$ pursues a spaceship passing at constant velocity $v>u$, accelerating with constant proper acceleration $a$. Find (a) the pursuit duration on the criminal's clock, (b) on the officer's clock, and (c) the relative velocity at catch-up.
Setup
The officer (subscript $p$) starts at rest in $S$ at $t=0$ and undergoes hyperbolic motion with constant proper acceleration $a$. The criminal (subscript $c$) cruises at constant velocity $v > 0$ along $+\hat x$. We parametrise by the officer's rapidity $\eta_p = a\tau_p/c$ (where $\tau_p$ is the officer's proper time).
Officer's worldline
Hyperbolic motion is the integral of $\dot x = c\tanh\eta_p,\;\gamma_p = \cosh\eta_p$, giving
$$t_S = \frac{c}{a}\sinh\eta_p,\qquad x_S = \frac{c^2}{a}(\cosh\eta_p - 1).$$
Catch-up condition
Criminal at $x = v t$. Set $x_S = v\,t_S$:
$$\frac{c^2}{a}(\cosh\eta_p - 1) = v\cdot\frac{c}{a}\sinh\eta_p \;\Longrightarrow\; \frac{\cosh\eta_p - 1}{\sinh\eta_p} = \frac{v}{c}.$$
Half-angle identities: $\cosh\eta_p - 1 = 2\sinh^2(\eta_p/2)$ and $\sinh\eta_p = 2\sinh(\eta_p/2)\cosh(\eta_p/2)$, so
$$\tanh(\eta_p/2) = v/c = \tanh\eta,\quad\text{where}\quad \eta \equiv\operatorname{arctanh}(v/c).$$
$$\boxed{\;\eta_p = 2\eta.\;}$$
(a) Criminal's proper time
$\tau_c = t_S/\gamma_v$ where $\gamma_v = \cosh\eta$ and $t_S = (c/a)\sinh(2\eta) = (2c/a)\sinh\eta\cosh\eta$:
$$\boxed{\;\tau_c = \frac{2c\sinh\eta}{a} = \frac{2v\gamma_v}{a}.\;}$$
(b) Officer's proper time
$$\tau_p = c\eta_p/a = 2c\eta/a = \boxed{\;\frac{c}{a}\ln\!\frac{c+v}{c-v}.\;}$$
(c) Relative velocity at catch-up
Rapidities subtract along boost-aligned worldlines: $\eta_\text{rel} = \eta_p - \eta = 2\eta - \eta = \eta$, so
$$\boxed{\;v_\text{rel} = c\tanh\eta = v.\;}$$
The officer catches the criminal moving relative to him at exactly the criminal's $S$-speed — a clean consequence of additive rapidities. In Newtonian mechanics with constant acceleration, $v_\text{rel}$ at catch-up would equal $v$ as well (officer reaches twice the criminal's speed), but only the rapidity formulation makes this transparent relativistically.
Rindler coordinates: metric, photon 4-wavevector, proper time
$t = X\sinh(aT)$, $x = X\cosh(aT)$, $y=Y$, $z=Z$. (a) Metric in $(T,X,Y,Z)$. (b) Components of $k^\mu = (\omega, \omega\cos\theta, 0, \omega\sin\theta)$ in Rindler coords at $(t_0,x_0,0,0)$. (c) Proper time on $X = X_0$, $Y = vT$, $Z = 0$, $T\in[0,T_0]$.
(a) The Rindler metric
Differentiate the coordinate transformation:
$$dt = \sinh(aT)\,dX + aX\cosh(aT)\,dT,\quad dx = \cosh(aT)\,dX + aX\sinh(aT)\,dT.$$
Substitute into $ds^2 = dt^2 - dx^2 - dy^2 - dz^2$:
$$dt^2 - dx^2 = a^2 X^2(\cosh^2 - \sinh^2)\,dT^2 - (\cosh^2 - \sinh^2)\,dX^2 + (\text{cross terms})\cdot 2\sinh\cosh\,(dT\,dX).$$
The cross terms have coefficient $aX\sinh\cosh\cdot\cosh - aX\cosh\cdot\sinh = 0$. Using $\cosh^2 - \sinh^2 = 1$:
$$\boxed{\;ds^2 = a^2 X^2\,dT^2 - dX^2 - dY^2 - dZ^2.\;}$$
The time-time component $g_{TT} = a^2 X^2$ depends on $X$ — gravitational redshift between Rindler observers, the equivalence-principle prototype for Unruh and Hawking radiation.
(b) Photon 4-wavevector in Rindler coordinates
Apply the Jacobian $\partial(T,X)/\partial(t,x)$ at the event $(t_0,x_0)$, equivalent to $(T_0,X_0)$ with $t_0 = X_0\sinh(aT_0)$, $x_0 = X_0\cosh(aT_0)$:
$$\frac{\partial T}{\partial t} = \frac{\cosh(aT_0)}{aX_0},\quad \frac{\partial T}{\partial x} = -\frac{\sinh(aT_0)}{aX_0},\quad \frac{\partial X}{\partial t} = -\sinh(aT_0),\quad \frac{\partial X}{\partial x} = \cosh(aT_0).$$
Acting on $k^\mu = (\omega,\omega\cos\theta,0,\omega\sin\theta)$ in Minkowski coordinates:
$$\boxed{\;k'^T = \frac{\omega[\cosh(aT_0) - \cos\theta\sinh(aT_0)]}{aX_0},\quad k'^X = \omega[\cos\theta\cosh(aT_0) - \sinh(aT_0)],\quad k'^Y = 0,\quad k'^Z = \omega\sin\theta.\;}$$
The $1/(aX_0)$ in $k'^T$ is the Rindler redshift in disguise: observers at large $X$ see lower frequency.
(c) Proper time on the worldline
With $X = X_0$, $Y = vT$, $Z = 0$: $dX = 0$, $dY = v\,dT$, so
$$d\tau^2 = (a^2 X_0^2 - v^2)\,dT^2.$$
Integrating from $T=0$ to $T_0$:
$$\boxed{\;\tau = T_0\sqrt{a^2 X_0^2 - v^2}.\;}$$
Real proper time requires $v < aX_0$ — the local Rindler speed limit. The Rindler horizon at $X = 0$ would force $\tau \to 0$, signaling the boundary of the accelerated wedge.
Hyperbolic motion: coordinate acceleration $a'$ in moving frame at $t'=0$
Worldline $t^2 - x^2 = -1/\alpha^2$. Boost to $S'$ at velocity $v$. Find $a'$ at $t' = 0$.
Locate the event $t'=0$ on the worldline
The boost $t' = \gamma(t - vx)$ gives $t' = 0 \iff t = vx$. Substituting into $t^2 - x^2 = -1/\alpha^2$:
$$v^2 x^2 - x^2 = -1/\alpha^2 \;\Longrightarrow\; x^2(1-v^2) = 1/\alpha^2 \;\Longrightarrow\; x = \gamma/\alpha,\quad t = v\gamma/\alpha.$$
Lab velocity and acceleration at that event
From $t^2 - x^2 = -1/\alpha^2$, differentiate: $t = x\dot x$ so $\dot x = t/x = v$ — the particle is momentarily at rest in $S'$. Differentiate again: $1 = \dot x^2 + x\ddot x = v^2 + (\gamma/\alpha)\ddot x$, giving
$$\ddot x = \frac{1-v^2}{\gamma/\alpha} = \frac{\alpha}{\gamma^3}.$$
Transform to $S'$
Coordinate acceleration transforms as $a' = \ddot x/[\gamma^3(1 - v\dot x)^3]$ (derived from boosting $dv/dt$). With $\dot x = v$: $(1 - v\dot x)^3 = (1-v^2)^3 = 1/\gamma^6$, so
$$a' = \gamma^3\cdot\frac{\alpha}{\gamma^3}\cdot\gamma^6\cdot\frac{1}{\gamma^6} = \alpha.$$
Wait — cleaner: $a' = \ddot x/[\gamma^3(1-v\dot x)^3] = (\alpha/\gamma^3)/[\gamma^3 \cdot 1/\gamma^6] = (\alpha/\gamma^3)\cdot(\gamma^3) = \alpha$.
$$\boxed{\;a' = \alpha.\;}$$
This is the definition of proper acceleration $\alpha$: the acceleration measured in the instantaneous rest frame. Equivalence-principle backbone of GR — Rindler observers feel constant $\alpha$, indistinguishable locally from a uniform gravitational field.
Light signal to an accelerating observer: Rindler horizon
$A,B$ colocated at rest. At lab time $0$, $B$ accelerates with proper acceleration $\alpha$. At lab time $t_0$, $A$ sends a light signal. Find $B$'s proper time at reception.
Setup
Hyperbolic motion with proper acceleration $\alpha$ starting from rest at the origin has worldline
$$x_B(t) = \sqrt{1/\alpha^2 + t^2} - 1/\alpha\,,\quad t\ge 0$$
(so that $x_B(0) = 0$, $\dot x_B(0) = 0$, $\alpha_\text{proper} = \alpha$). Light signal sent from $A$ at lab time $t_0$ travels along $x = t - t_0$.
Intersection
Set $x_B(t) = t - t_0$:
$$\sqrt{1/\alpha^2 + t^2} = t - t_0 + 1/\alpha.$$
Square both sides ($t > t_0$ for the signal to reach $B$):
$$1/\alpha^2 + t^2 = (t - t_0 + 1/\alpha)^2.$$
Expanding: $t^2 + 1/\alpha^2 = t^2 - 2t(t_0 - 1/\alpha) + (t_0 - 1/\alpha)^2$, which gives
$$t_\text{rec} = \frac{(t_0 - 1/\alpha)^2 - 1/\alpha^2}{2(t_0 - 1/\alpha)}\cdot(-1) \cdot\frac{1}{1} = \frac{t_0(2/\alpha - t_0)}{2(1/\alpha - t_0)} = \frac{t_0(2 - \alpha t_0)}{2\alpha(1-\alpha t_0)/\alpha^2}\cdot\alpha = \frac{t_0(2-\alpha t_0)}{2(1-\alpha t_0)}\cdot\frac{1}{1}.$$
Cleanly: $t_\text{rec} = t_0(2-\alpha t_0)/[2(1-\alpha t_0)]$, real and positive only when $\alpha t_0 < 1$.
Convert to $B$'s proper time
For hyperbolic motion, $\tau_B = \alpha^{-1}\sinh^{-1}(\alpha t)$. Therefore
$$\boxed{\;\tau_B = \frac{1}{\alpha}\sinh^{-1}\!\left[\frac{\alpha t_0(2 - \alpha t_0)}{2(1 - \alpha t_0)}\right],\quad t_0 < 1/\alpha.\;}$$
The Rindler horizon
For $t_0 \ge 1/\alpha$: $t_0$ lies on or beyond the asymptotic null ray $x = t - 1/\alpha$ that the worldline approaches but never crosses. The light signal lies in the part of Minkowski space outside the Rindler wedge — it never reaches $B$.
This is the equivalence-principle analogue of a black-hole event horizon. With quantum vacuum fluctuations, the same redshift structure generates thermal Unruh radiation at $T = \alpha\hbar/(2\pi k_B c)$, exactly mirroring Hawking radiation at the Schwarzschild horizon.
Circular accelerator: 4-acceleration, proper acceleration, eigentime per orbit
Particle in circular orbit at radius $R$, constant speed $v$, $\gamma$ constant. Find the 4-acceleration magnitude and proper time per orbit.
Worldline and 4-velocity
Choose lab coordinates so the orbit lies in the $xy$-plane: $\vec x(t) = R(\cos\omega t, \sin\omega t, 0)$ with angular frequency $\omega = v/R$. Lab velocity $\vec u = R\omega(-\sin\omega t,\cos\omega t,0)$ has constant magnitude $|\vec u| = v$, so $\gamma$ is constant. The 4-velocity:
$$U^\mu = \gamma\bigl(c,\; v(-\sin\omega t, \cos\omega t, 0)\bigr).$$
4-acceleration
$A^\mu = dU^\mu/d\tau = \gamma\,dU^\mu/dt$. Time-derivative of the spatial part: $-\gamma v\omega(\cos\omega t,\sin\omega t,0) = -\gamma v\omega\,\hat r$. So
$$A^\mu = \gamma\bigl(0,\;-\gamma v\omega\hat r\bigr) = (0,\;-\gamma^2 v\omega\,\hat r).$$
Magnitude (spacelike, since $A\!\cdot\!U = 0$):
$$|\vec A| = \gamma^2 v\omega = \gamma^2 v^2/R.$$
Proper acceleration and orbital proper period
The magnitude of the 4-acceleration is the proper acceleration:
$$\boxed{\;\alpha = \gamma^2 v^2/R.\;}$$
Lab period $T_\text{lab} = 2\pi R/v$. Proper period contracts:
$$\boxed{\;T_\text{proper} = T_\text{lab}/\gamma = \frac{2\pi R}{\gamma v}.\;}$$
Physical interpretation
The Newtonian centripetal acceleration is $v^2/R$; the proper value is enhanced by $\gamma^2$ — the relativistic-mass enhancement of effective inertia. At LEP ($e^-$ at 100 GeV, $\gamma\sim 2\times 10^5$, $R\approx 4.3$ km), $\alpha \sim 4\times 10^{14}$ m/s² in the electron's own frame — producing copious synchrotron radiation. Same physics as Problem 1.15 (muon storage rings): $1/\gamma$ proper-period gives many lab orbits per proper lifetime.
Force parallel to worldline: $dM/d\tau = f$, $\alpha = 0$
Object of internal energy $M$ acted on by $F = fU$ with $U^2 = 1$. Find $dM/d\tau$ and proper acceleration.
The 4-force decomposition
For a particle whose internal energy $M$ can change, the relativistic Newton equation reads
$$F^\mu = \frac{d(M U^\mu)}{d\tau} = \frac{dM}{d\tau}U^\mu + M\,\frac{dU^\mu}{d\tau} = \frac{dM}{d\tau}U^\mu + MA^\mu,$$
where $A^\mu = dU^\mu/d\tau$ is the 4-acceleration. Since $U\!\cdot\!U = c^2$ is constant, $A\!\cdot\!U = 0$ — the 4-acceleration is always orthogonal to the 4-velocity.
Projection onto $U$
Take the inner product with $U_\mu$:
$$F\!\cdot\!U = \frac{dM}{d\tau}\,U\!\cdot\!U + M\,A\!\cdot\!U = \frac{dM}{d\tau}\cdot c^2 + 0.$$
(Here I set $c=1$ to match the problem statement, so $U\!\cdot\!U = 1$.) Given $F = fU$: $F\!\cdot\!U = f\,U\!\cdot\!U = f$. Therefore
$$\boxed{\;\frac{dM}{d\tau} = f.\;}$$
Projection orthogonal to $U$
From the decomposition: $MA^\mu = F^\mu - (dM/d\tau)U^\mu = fU^\mu - fU^\mu = 0$, so
$$\boxed{\;A^\mu = 0,\quad\alpha = 0.\;}$$
Physical interpretation
A 4-force parallel to $U$ deposits all its energy as rest mass (internal heating, excitation) — no trajectory bending. The particle continues on a geodesic of Minkowski space while its rest energy grows linearly with proper time. Examples: thermal absorption in a thin opaque target moving with the particle; gain of binding energy without ejecta.
Duality. Compare with Problem 1.53 (4-force purely spatial, $F = (0,\vec b)$): all energy goes to acceleration, none to mass change — the orthogonal projection.
4-force $F = (0,\vec b)$: rate of mass change, pure-force condition
4-force $F^\mu = (0,\vec b)$ on a particle with 3-velocity $\vec u$, rest energy $m$. Find $dm/d\tau$, proper acceleration, and the pure-force condition.
Compute $F\!\cdot\!U$
With $U^\mu = \gamma(c, \vec u)$ and $F^\mu = (0,\vec b)$:
$$F\!\cdot\!U = F^\mu U_\mu = 0\cdot\gamma c - \vec b\!\cdot\!\gamma\vec u = -\gamma\vec b\!\cdot\!\vec u.$$
(With signature $(+,-,-,-)$; for $(-,+,+,+)$ the sign flips, but the physics is the same.) Using the Problem 1.52 derivation $F\!\cdot\!U = c^2\,dm/d\tau$ (with $M\to m$):
$$\boxed{\;\frac{dm}{d\tau} = \frac{\vec b\!\cdot\!\vec u\,\gamma}{c^2}.\;}$$
Proper acceleration
Decompose $F^\mu = (dm/d\tau)U^\mu + mA^\mu$. In the instantaneous rest frame, $\vec u = 0$, so $dm/d\tau = 0$ and $F^\mu_\text{rest} = mA^\mu_\text{rest}$. The spatial part of $F^\mu$ in the rest frame is $\vec b_\text{rest}$, with magnitude $|\vec b_\text{rest}| = |\vec b|$ (since the spatial part of a 4-vector with $F^0 = 0$ in some frame is not Lorentz-invariant in magnitude in general — but for this specific configuration $F\!\cdot\!F = -|\vec b|^2$ is invariant). So
$$\boxed{\;\alpha = |\vec b|/m.\;}$$
Pure-force condition
"Pure" means $dm/d\tau = 0$ — all the 4-force goes into acceleration, none into mass change. This requires
$$\vec b\!\cdot\!\vec u = 0 \;\Longleftrightarrow\; \vec b\perp\vec u.$$
Magnetic force example
The magnetic Lorentz 3-force is $\vec b = q\vec u\times\vec B$, which automatically satisfies $\vec b\!\cdot\!\vec u = q(\vec u\times\vec B)\!\cdot\!\vec u = 0$. So magnetic forces are exactly pure forces: $dm/d\tau = 0$ — magnetic forces never do work. The covariant version: the Lorentz 4-force $F^\mu = qF^{\mu\nu}U_\nu$ satisfies $F\!\cdot\!U = qF^{\mu\nu}U_\mu U_\nu = 0$ by antisymmetry of $F^{\mu\nu}$. Dual to Problem 1.52 (parallel force = pure mass change).
Acceleration in lab given proper acceleration $a_0$
Object has acceleration $a_0$ at angle $\theta$ to boost direction in its instantaneous rest frame. Find lab acceleration; min/max as function of $\theta$.
Acceleration transformation formulae
The general transformation of 3-acceleration from rest frame to lab is
$$a'_\parallel = \frac{a_\parallel}{\gamma^3(1 - vu_\parallel/c^2)^3},\qquad a'_\perp = \frac{a_\perp + (v/c^2)(\vec u\times\vec a)_\perp\,(\dots)}{\gamma^2(1 - vu_\parallel/c^2)^3}.$$
In the instantaneous rest frame $\vec u = 0$, so the $(1 - vu_\parallel/c^2)^3 = 1$ factor disappears. The rest-frame components of proper acceleration $a_0$ at angle $\theta$ to the boost direction are $a_\parallel = a_0\cos\theta$, $a_\perp = a_0\sin\theta$, so
$$a'_\parallel = \frac{a_0\cos\theta}{\gamma^3},\quad a'_\perp = \frac{a_0\sin\theta}{\gamma^2}.$$
Lab-frame magnitude
$$|a'|^2 = a'^2_\parallel + a'^2_\perp = \frac{a_0^2\cos^2\theta}{\gamma^6} + \frac{a_0^2\sin^2\theta}{\gamma^4} = \frac{a_0^2}{\gamma^4}\left[\frac{\cos^2\theta}{\gamma^2} + \sin^2\theta\right].$$
Combine using $1/\gamma^2 = 1 - \beta^2$: $\cos^2\theta/\gamma^2 + \sin^2\theta = (1-\beta^2)\cos^2\theta + \sin^2\theta = 1 - \beta^2\cos^2\theta$. Therefore
$$\boxed{\;a'(\theta) = \frac{a_0}{\gamma^2}\sqrt{1 - \beta^2\cos^2\theta}.\;}$$
Extrema
The quantity $1-\beta^2\cos^2\theta$ runs between $1-\beta^2 = 1/\gamma^2$ (at $\theta=0$) and $1$ (at $\theta = \pi/2$):
$$\boxed{\;\frac{a_0}{\gamma^3}\le a'\le\frac{a_0}{\gamma^2},\quad\text{min at }\theta=0,\;\max\text{ at }\theta=\pi/2.\;}$$
Interpretation
Lab acceleration is always smaller than proper acceleration — "relativistic mass" enhancement makes objects harder to accelerate. The longitudinal direction is more suppressed ($\gamma^3$) than transverse ($\gamma^2$): along the boost the time-dilation effect compounds with the parallel velocity addition. Proper acceleration is what the particle's own accelerometer reads — the basis for the equivalence-principle interpretation in GR.