Undergraduate Antenna Engineering

Parabolic Reflector Antennas Study Guide

Theory, design principles, and applications of high-gain directional antennas. From satellite communications to radio astronomy.

Focal Point Parabolic Surface Aperture

High Gain

Achieve gains of 30-50 dBi with narrow beamwidths, ideal for long-distance communication links.

Geometric Optics

Based on the paraboloid property: all rays from focus reflect parallel to the axis (and vice versa).

Wide Applications

Satellite communications, radio astronomy, radar systems, and deep space networks.

Fundamental Theory

Understanding the physics and mathematics behind parabolic reflectors

The Paraboloid Geometry

A parabolic reflector is formed by rotating a parabola about its axis. The standard equation in Cartesian coordinates:

x² = 4fz

Where f is the focal length. In cylindrical coordinates (ρ, φ, z):

ρ² = 4fz

The f/D ratio (focal length to diameter ratio) is crucial for design, typically ranging from 0.25 to 0.5.

Key Property: Equal Path Lengths

The defining characteristic of a parabola is that any ray emanating from the focus reflects off the surface and travels parallel to the axis. Conversely, incoming parallel rays converge at the focus.

  • Path length from focus to surface to aperture plane is constant for all rays
  • This ensures phase coherence across the aperture
  • Results in plane wave formation in the far field

Aperture Illumination

The feed antenna illuminates the reflector with a specific pattern. The aperture field distribution determines:

  • Beamwidth: Inversely proportional to aperture diameter
  • Sidelobe levels: Depend on taper distribution
  • Efficiency: Affected by spillover and illumination taper

Interactive Ray Diagram

Shallow (0.25) Deep (0.6)
Observation: As f/D increases, the dish becomes shallower and the feed illumination angle decreases.

G Gain Calculation

Ideal Gain (no losses):

G = (πD/λ)²

With Aperture Efficiency (η):

G = η(πD/λ)²

In dBi:

G(dBi) = 10log₁₀[η(πD/λ)²]

Typical aperture efficiency η ranges from 0.5 to 0.7 (50-70%) due to spillover, blockage, and non-uniform illumination.

θ Beamwidth Calculation

Half-Power Beamwidth (HPBW):

θ₃dB ≈ 70λ/D (degrees)

Null-to-Null Beamwidth:

θ_null ≈ 140λ/D (degrees)

First Sidelobe Level (uniform illumination):

-17.6 dB

Beamwidth is inversely proportional to diameter. Larger dishes produce narrower beams, requiring precise pointing.

Feed Systems & Illumination

Dipole Feed

Dipole with Reflector

Simple half-wave dipole backed by a small plane reflector. Used for small parabolic dishes.

  • • Simple construction
  • • Moderate bandwidth
  • • Typical for f/D ≈ 0.4
Horn Feed

Pyramidal/Conical Horn

Most common feed for parabolic reflectors. Provides controlled illumination pattern.

  • • Low sidelobes
  • • High efficiency
  • • Adjustable beamwidth
Cassegrain

Cassegrain (Dual Reflector)

Hyperbolic subreflector allows feed to be placed at the vertex. Shorter mechanical structure.

  • • Reduced feed line loss
  • • Convenient access
  • • Lower noise temperature

Feed Illumination Patterns

Illumination Taper

The feed pattern must illuminate the reflector edge at a lower level than the center (typically -10 to -12 dB). This taper:

  • Reduces sidelobe levels
  • Increases aperture efficiency
  • But reduces effective aperture area

Edge Taper Trade-off: -10 dB edge taper typically gives ~80% illumination efficiency with -20 dB first sidelobes.

Interactive Design Calculator

Parameters

Performance Metrics

Wavelength

30 mm

Gain

38.1 dBi

3dB Beamwidth

1.4°

Focal Length

0.60 m

Depth at Center

0.35 m

Half-Angle

64°

Geometry Preview

Radiation Pattern (Far Field)

E-Plane
H-Plane

Real-World Applications

Satellite Communications

VSAT terminals, DBS reception, and earth station antennas. Diameters: 0.6m to 30m.

C, Ku, Ka Bands

Radio Astronomy

Jansky Very Large Array, Arecibo (305m), Green Bank Telescope (100m).

100 MHz - 100 GHz

Radar Systems

Air traffic control, weather radar, and military tracking systems.

L, S, C, X Bands

Deep Space Network

NASA's 70m dishes for interplanetary communication with spacecraft.

S, X, Ka Bands

Case Study: NASA Deep Space Network

The Deep Space Network (DSN) uses 70-meter parabolic antennas to communicate with distant spacecraft. These massive dishes feature:

  • 1 Beamwidth: 0.04° at X-band (8.4 GHz) - narrower than the angular diameter of Mars at closest approach
  • 2 Gain: ~74 dBi at X-band, capable of detecting signals from billions of kilometers away
  • 3 Surface Accuracy: Within 0.5 mm RMS to maintain efficiency at millimeter wavelengths
70m

Diameter

74 dBi

Gain at X-band

0.04°

Beamwidth

Essential Equations Summary

Geometry

Parabola equation: ρ² = 4fz

Depth: h = D²/(16f)

Half-angle: ψ₀ = 2arctan(D/4f)

Surface area: A = (πD⁴)/(64f²) [approx]

Electrical

Gain: G = η(πD/λ)²

Beamwidth: θ₃dB ≈ 70λ/D

Directivity: D₀ = (πD/λ)²

Effective area: Ae = ηAphysical

Feed Design

Edge taper: ET = 20log₁₀(Cosⁿ(ψ₀))

Spillover efficiency: ηs = ∫∫|E|²dΩ / Ptotal

Taper efficiency: ηt = [∫∫E dA]² / [A∫∫|E|²dA]

Link Budget

Free space path loss: FSPL = (4πR/λ)²

Received power: Pr = PtGtGrλ²/(4πR)²

Antenna noise: Ta = Tground + Tsky + Tspill

Study Checklist