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Multimode vs single mode; NA derivation

Short answer

Multimode fibre has larger core, easier LED launch, cheaper connectors and lower system cost, but suffers high intermodal dispersion, high attenuation, and short reach. NA for step-index fibre is derived from Snell's law and TIR condition: NA = n0 sin θa = sqrt(n1^2 - n2^2) ≈ n1 sqrt(2Δ).

What are advantages and disadvantages of multimode fiber over single mode fiber? Derive expression of Numerical Aperture of a stepped index optical fiber.

Multimode fibre compared with single mode fibre

Advantages of multimode fibre

  • Larger core (50–200 µm) and larger NA, so light can be launched from cheap LEDs.
  • Easier and cheaper splicing, connectors and alignment.
  • Lower total system cost for short links (LANs, buildings, campuses).
  • Can be used with low-cost sources at 850 nm.

Disadvantages of multimode fibre

  • Large intermodal dispersion, so low bandwidth (MHz·km to about 1 GHz·km).
  • Higher attenuation than single mode fibre.
  • Short maximum link length; not suitable for long-haul or high-speed WDM systems.

Derivation of NA of a step-index fibre

Consider a step-index fibre with core index n1n_1, cladding index n2n_2 (n1>n2n_1 > n_2), and outside medium index n0n_0 (air, n0=1n_0 = 1). A meridional ray enters the core end at angle θ0\theta_0 to the axis.

        n0  |    cladding n2
   ray \    |__________________
        \th0|   /\phi
 axis ---*--+--/--\----------- core n1
            |th1   \
            |__________________
              cladding n2

Step 1: refraction at the input face. By Snell's law:

n0sin⁡θ0=n1sin⁡θ1n_0\sin\theta_0 = n_1\sin\theta_1

Step 2: angle at the core–cladding boundary. The refracted ray meets the boundary at angle ϕ\phi to the normal. From the right-angled triangle:

ϕ=90∘−θ1⇒sin⁡θ1=cos⁡ϕ\phi = 90^\circ - \theta_1 \quad\Rightarrow\quad \sin\theta_1 = \cos\phi

Step 3: condition for total internal reflection. The ray is guided only if ϕ≥ϕc\phi \ge \phi_c, where the critical angle is given by

sin⁡ϕc=n2n1\sin\phi_c = \frac{n_2}{n_1}

Step 4: maximum acceptance angle. The largest input angle θ0=θa\theta_0 = \theta_a corresponds to ϕ=ϕc\phi = \phi_c:

n0sin⁡θa=n1sin⁡θ1=n1cos⁡ϕc=n11−sin⁡2ϕc=n11−n22n12=n12−n22\begin{aligned} n_0\sin\theta_a &= n_1\sin\theta_1 = n_1\cos\phi_c \\ &= n_1\sqrt{1 - \sin^2\phi_c} \\ &= n_1\sqrt{1 - \frac{n_2^2}{n_1^2}} \\ &= \sqrt{n_1^2 - n_2^2} \end{aligned}

Step 5: definition of NA.

NA=n0sin⁡θa=n12−n22\text{NA} = n_0\sin\theta_a = \sqrt{n_1^2 - n_2^2}

For air, NA=sin⁡θa\text{NA} = \sin\theta_a and θa=sin⁡−1n12−n22\theta_a = \sin^{-1}\sqrt{n_1^2 - n_2^2}.

Step 6: in terms of relative index difference. With Δ=n12−n222n12≈n1−n2n1\Delta = \dfrac{n_1^2 - n_2^2}{2n_1^2} \approx \dfrac{n_1 - n_2}{n_1} (since n1≈n2n_1 \approx n_2):

n12−n22=2n12Δ⇒NA=n12Δn_1^2 - n_2^2 = 2n_1^2\Delta \quad\Rightarrow\quad \text{NA} = n_1\sqrt{2\Delta}

Example: n1=1.48n_1 = 1.48, n2=1.46n_2 = 1.46:

NA=1.482−1.462=0.0588=0.2425θa=sin⁡−1(0.2425)=14.03∘\begin{aligned} \text{NA} &= \sqrt{1.48^2 - 1.46^2} = \sqrt{0.0588} = 0.2425 \\ \theta_a &= \sin^{-1}(0.2425) = 14.03^\circ \end{aligned}

NA depends only on the refractive indices, not on the core diameter. The full acceptance cone angle is 2θa2\theta_a.

✓ Answer checked by Claude Opus 5.5 (high effort)

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