- 2075 Bhadra · 2+8 marks
MUF, critical frequency and skip (curved earth)
Short answer
MUF is the highest frequency reflected between two points for a given angle of incidence. f_MUF = fcr sec φ with fcr = 9√Nmax (critical frequency). For curved earth, tan φ = R sin(D/2R)/(R+h−R cos(D/2R)), and skip distance D = (2R/k)[1−√(1−2k²h/R)] with k = √((f/fcr)²−1).
What is Maximum Usable Frequency (MUF)? Derive the expression of MUF, critical frequency (fcr) and skip distance assuming curved earth.
Maximum Usable Frequency (MUF)
The MUF is the highest frequency that is returned to earth by the ionosphere between two given points (for a given angle of incidence). Higher frequencies pass through the layer. It is related to the critical frequency fcr (highest frequency reflected at vertical incidence) by the secant law: f_MUF = fcr sec φ. In practice the optimum working frequency OWF ≈ 0.85 MUF is used.
Derivation for curved earth
Assumptions: spherical earth of radius R; layer acting as a thin reflector at virtual height h; both antennas on the ground; reflection point P above the mid-point of the path.
First, the secant law. The refractive index of the layer is n = √(1 − 81N/f²). By Snell's law, a ray entering at angle φ returns where n = sin φ:
1 − 81Nmax/f² = sin² φ
81Nmax/f² = cos² φ
f = 9√Nmax / cos φ = fcr sec φ, fcr = 9√Nmax
Then the curved-earth geometry:
P (reflection point, height h)
/|\
/ | \ φ = angle of incidence at P
/φ | \
~~~~~~~~/~~~|~~~\~~~~~~~ ionosphere
T / | \ R (on earth surface)
\. | ./
`. |θ .' θ = D / (2R)
`. | .'
O (earth centre)
OT = R, OP = R + h, arc TR = D
Step 1: Drop a perpendicular from T onto OP. Its foot Q lies at distance R cos θ from O, and TQ = R sin θ. In triangle TQP:
QP = (R + h) − R cos θ
tan φ = TQ / QP = R sin θ / (R + h − R cos θ)
Step 2: Secant law for the ionosphere (from n = √(1 − 81N/f²) and Snell's law): f_MUF = fc sec φ, with fc = 9√Nmax. So:
f_MUF = fc √(1 + tan² φ)
f_MUF = fc √{ 1 + [ R sin(D/2R) /
(R + h − R cos(D/2R)) ]² }
Step 3: For D small compared with R, sin θ ≈ θ = D/2R and cos θ ≈ 1 − θ²/2:
tan φ ≈ (D/2) / (h + D²/8R)
f_MUF ≈ fc √{ 1 + [ (D/2) / (h + D²/8R) ]² }
Step 4: Skip distance for a given frequency f. Let k = √[(f/fc)² − 1] = tan φ:
D/2 = k (h + D²/8R)
(k/8R) D² − D/2 + k h = 0
D = (2R/k) [ 1 − √(1 − 2k²h/R) ] (smaller root)
Check: as R → ∞, √(1 − x) ≈ 1 − x/2, so D → 2kh = 2h√[(f/fc)² − 1], the flat-earth result.
Step 5: Limit due to curvature. The largest angle φ occurs when the ray leaves the transmitter along the horizon (tangent at T):
sin φmax = R / (R + h)
f_MUF(max) = fc sec φmax
D_max (one hop) = 2R cos⁻¹[R / (R + h)]
For h = 300 km, R = 6370 km: sin φmax = 0.955, φmax = 72.8°, sec φmax = 3.37, D_max ≈ 3836 km. So single-hop MUF cannot exceed about 3.4 fc.
Summary
fcr = 9 √Nmax
f_MUF = fcr sec φ,
tan φ = R sin(D/2R) / (R + h − R cos(D/2R))
D = (2R/k)[1 − √(1 − 2k²h/R)], k = √[(f/fcr)² − 1]
Example: fcr = 8 MHz, h = 300 km, f = 16 MHz: k = √3 = 1.732; D = (2 × 6370/1.732)[1 − √(1 − 2 × 3 × 300/6370)] ≈ 1125 km (the flat-earth formula gives 1039 km).
✓ Answer checked by Claude Opus 5.5 (high effort)
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