[rev 09.17.09.00.10]
VHF - UHF basics by KE9SE
This page is intended to be an introduction to and provide a basic understanding of VHF and UHF radio communications. The information was compiled from many sources and a bibliography will be included at the end. Although the information is directly related, it was discovered that a lot of hunting was required to bring it all together. So the second purpose of this page is to be a one stop information resource, one which hopefully you will find to be convenient and helpful. All of the math used in these examples is simple and can be solved using the Windows calculator in the scientific mode. Care must be taken to solve the operations within the parenthesis, a scratch pad helps keep things in order. Because of a likeness for RPN and the convenience of the stack, I prefer to use an HP-48.
This page is not complete and probably never will be. It will however be updated and corrected as time permits. If a listed topic has not been developed yet, it eventually will be. Please feel free to email any suggestions, improvements or hate mail to me:
Kelvin to Celsius C° = K° - 273.15
Celsius to Fahrenheit F˚ = ( 9 / 5 • C˚ ) + 32
Fahrenheit to Celsius C˚ = 5 / 9 • ( F˚ - 32 )
The decibel is logarithmic in nature and represents a ratio. The dB is a convenient way to sum losses and gains.
dBW = a value relative to 1 watt 0 dBW = 30 dBm
dBm = a value relative to 1 milliwatt 0 dBm = -30 dBW
Examples:
-10 dBm = 1/10 of a milliwatt
-20 dBm = 1/100 of a milliwatt
-30 dBm = 1/1000 of a milliwatt
S9 +60dB = 1/20 of a milliwatt
dBi = gain relative to an isotropic antenna model
dBd = gain relative to a half wave dipole antenna
0 dBd = 2.14 dBi
An isotropic radiator has a spherical radiation pattern, it will transmit an equal amount of energy to all points within a sphere. The isotropic radiator is a purely mathematical construct and is presently not possible to build. So why bother referencing to it? It is an absolute platform of reference which gives it scientific value.
Some antenna manufacturers inflate their gain claims by using dBi rather than dBd and others will even include fresnel ground reflection (ground bounce) as a function of antenna gain, this is not a lie but is misleading. The effects of the ground on an antenna pattern vary with terrain, antenna height, ground conductivity and dielectric constant. Ground bounce characteristics change with local climate, it is difficult to predict or model these effects with absolute accurately (unless you live on a flat metal surface, many wavelengths in radius).
Decibel value from a voltage or current ratio dB = 20 x ( Log10 ( V1 / V2 ))
Converting a decibel value to a power ratio PR = Antilog10 ( dB / 10 )
Converting a decibel value to a voltage ratio VR = Antilog10 ( dB / 20 )
| dB | power ratio | voltage or current ratio | dB | power ratio | voltage or current ratio |
| 0 | 1.00 | 1.00 | 10 | 10 | 3.16 |
| 0.5 | 1.12 | 1.06 | 15 | 31.6 | 5.62 |
| 1.0 | 1.26 | 1.12 | 20 | 100 | 10 |
| 1.5 | 1.41 | 1.19 | 25 | 316 | 17.78 |
| 2.0 | 1.58 | 1.26 | 30 | 1000 | 31.6 |
| 3.0 | 2.00 | 1.41 | 40 | 10,000 | 100 |
| 4.0 | 2.51 | 1.58 | 50 | 100,000 | 316 |
| 5.0 | 3.16 | 1.78 | 60 | 106 | 1000 |
| 6.0 | 3.98 | 2.00 | 70 | 107 | 3,162 |
| 7.0 | 5.01 | 2.24 | 80 | 108 | 10,000 |
| 8.0 | 6.31 | 2.51 | 90 | 109 | 31,620 |
| 9.0 | 7.94 | 2.82 | 100 | 1010 | 105 |
Most of what we will be dealing with here will use the power ratio.
Noise is what places a limit on how weak of a signal we can detect, the signal to noise ratio or noise temperature is inversely proportional to sensitivity.
Thermal noise is the limiting factor of weak signal detection, it is a function of molecules in motion which can easily be calculated and because it is effected by bandwidth, an understanding of thermal noise (the theoretical noise floor) is useful. kTB is the formula used for determining the noise floor.
Pn = kTB
Pn = noise power in watts
k = Boltzman's constant (do not confuse with K)
k = 1.38 times 10 to the minus 23 joule per degree Kelvin
k = 1.38 x 10-23
T = temperature in degrees Kelvin (K)
B = bandwidth in hertz
T is typically seen as 290 degrees K in most examples, this corresponds to 17 degrees C which is about 62 degrees F
Therefore, a 1 hertz bandwidth has a noise floor of:
Pn = ((1.38 x 10-23) x 290) x 1
Pn = 0.000000000000000000004002 a rather useless number to me until it has been converted to a decibel
10 x (Log 0.000000000000000000004002) = -203.977 dBW (-204 dBW is close enough)
When referring to noise floor it is more customary to use dBm so simply subtract a minus 30 (change the sign of the subtrahend and add)
(-204) - (-30) = -174 dBm (per hertz)
How bandwidth is related to noise floor:
The width of the received pass band will have an effect upon the noise floor. There are two easy ways to derive the thermal noise floor for a given bandwidth. The first is to recalculate using the kTB formula and the second to "10 Log" the difference between two bandwidths.
Nf = 10 x ( Log10 ((1.38-23) x 290) x 12000)
Nf = 10 x ( Log10 (( 4.002-21) x 12000))
Nf = 10 x ( Log10 (4.8024-17))
Nf = 10 x ( -16.31854...)
Nf = -163 dBW
Nf = -133 dBm
Nf = 10 x ( Log10 ( Bw1 / Bw2 ))
Nf = 10 x ( Log10 12000 / 1 ))
Nf = 10 x ( Log10 12000)
Nf = 10 x (4.0791812460476...)
Nf = 40.79 dB (difference)
Since we know -174 dBm we combine +40.79 and the result is,
Nf = -133.21 dBm
Thermal noise floor for common bandwidths:
| Bandwidth | Thermal noise floor |
| 250 Hz | -151 dBm |
| 500 Hz | -147 dBm |
| 1 KHz | -144 dBm |
| 2 KHz | -141 dBm |
| 3 KHz | -139 dBm |
| 5 KHz | -137 dBm |
| 10 KHz | -134 dBm |
| 15 KHz | -132 dBm |
| 75 KHz | -125 dBm |
| 100 KHz | -124 dBm |
| 150 KHz | -122 dBm |
It would be nice if all receiving equipment was capable of receiving into the thermal noise floor. Unfortunately that's not the way the world works, there are many more sources of noise that we have to deal with.
Sky noise
Galactic noise
Sun noise
Antenna noise
Conversion from noise figure to noise temperature:
TE (expressed in degrees Kelvin) = 290 ( Antilog10 ( NF / 10 ) -1 )
TE = noise temperature
NF = noise figure
K degrees Kelvin
TE = 290 x ( Antilog10 ( 2.5 / 10 ) - 1)
TE = 290 x ( Antilog10 ( .25 ) - 1 )
TE = 290 x ( 1.778 - 1 )
TE = 290 x 0.778
TE = 225.62 K (degrees Kelvin)
Conversion from noise temperature to noise figure:
NF (expressed in dB) = 10 x Log10 ( 1 + ( TE / TO ))
NF = noise figure
TE = noise temperature
TO = 290 K ( degrees Kelvin )
NF = 10 x Log10 ( 1 + 80 / 290 )
NF = 10 x Log10 ( 1 + 0.27586 )
NF = 10 x Log10 ( 1.27586 )
NF = 10 x 0.1058 )
NF = 1.058 dB
The noise factor of a system or component is the ratio, a number greater than one, which corresponds to the equivalent noise figure. The noise figure is divided by 10 because we are dealing with a power ratio ( Pn ).
N (noise factor) = Antilog10 ( NF / 10 )
N = Antilog10 ( .25 )
N = 1.778 (or 1.778 : 1)
The purpose of the preamplifier is to increase the signal to noise ratio of the received signal. The preamplifier will possess some noise of its own, this is the noise figure of the amplifier. Generally for VHF a noise figure of 1 dB is more than adequate, for UHF a slightly lower noise figure may be needed to hear down into the ambient noise. The preamplifier gain needs only to overcome the downstream losses in the system. As an example, if the coaxial losses are equal to 2.5 dB and the selectivity device (cavity filter or whatever you prefer to use, if anything) has a loss of 1 dB and the front end of the receiver has a noise figure of 2 dB, then 5.5 dB gain will be all that is required of the preamplifier. This is called takeover gain. Any preamplifier gain beyond this point is called excess gain and will serve no purpose other than to inflate your receiver's S-meter, it will not increase the sensitivity of your receiver, lower the noise temperature of your system, or increase your signal to noise ratio (all one in the same).
Excess gain can also degrade receiver performance from the effects of gain compression and third order IMD products. IMD will become a problem if there are strong signals within the passband of your preamplifier.
There is a source of noise that is often overlooked because it is relatively small, that noise is produced from the heat within the lossy system component (coax for instance). The amplification of noise will raise the overall system temperature (example to be given in the future)
Since the purpose of the preamplifier is to increase the signal to noise ratio, it becomes obvious that it should have a low noise figure and it should be the first component after the antenna. By placing the preamp at the antenna feedpoint (or common connection to a stacking manifold) the noise barrier imposed by the coax losses and the amplified noise temperature derived from the lossy device itself is excluded. The only thermal noise that we have to contend with is the noise figure of the preamp itself. A coaxial relay is used to bypass the amplifier during transmission and to ground the input when not in use for static protection. The relay is best inserted into a logical "and" loop so that the transmitter will only key after all positive conditions have been met.
A resonant cavity filter at the input of the receiver can be used to clean up the preamplifier and protect the front end of the receiver from overloading and third order intermodulation products. The insertion loss of the pictured filter was measured using 100 watts at 146.475 MHz, a VHF watt/vswr meter and a 50 ohm dummy load.
The first measurement was made with the equipment in this order, ICOM 706, Mirage amplifier, VHF watt/swr meter, cavity filter, and dummy load. The cavity filter was tuned for minimum vswr and the power output adjusted to 100 watts.
The second measurement was made by placing the watt/swr meter between the cavity filter and the dummy load, a reading of 85 watts was observed. Interconnecting coaxial cables were kept as short as possible to reduce measurement errors due to lumped LC constants native to resonant lengths of coax.
The measured loss was 0.7 dB. The resulting signal-to-noise degradation (approximately the same as the loss 0.7dB) can be easily overcome by upstream takeover gain. The Q of the cavity is quite high so the receiver (Icom 706) is well protected from overloading. When transmitting, the missing 15 watts helps to heat the shack.

The pictured cavity filter, even though not 1/4 wavelength long, maintains a high Q through its gold plating both inside and out. Gold, although not quite as good of a conductor as silver or copper will not oxidize or corrode under normal use. Because of this, skin effect resistance remains low and will not degrade with age. The internal coupling loops are silver plated for highest efficiency and will not oxidize as long as the cavities remain assembled. The two filter sections are independently tunable and can be retuned when a frequency change of more than 300 KHz is made. These were purchased from Fair Radio Sales (Lima, Ohio). I do not know of the current availability.
Gain compression
Third order IMD products
dBc
RF selectivity
Detectors
SSB versus FM signal to noise ratio
For a reference, here is a table which will help you to compare received signal strength. Your mileage may vary depending upon your radio manufacturer. In most receivers the voltage used to power the S-meter is scaled from the agc voltage via a buffer or amplifier circuit. Although care is taken to tailor the gain and linearity (or non linearity) of the circuit, no two S-meters seem to act alike..
| S-0 | 0.1 uV | -127 dBm |
| S-1 | 0.2 uV | -121 dBm |
| S-2 | 0.4 uV | -115 dBm |
| S-3 | 0.8 uV | -109 dBm |
| S-4 | 1.58 uV | -103 dBm |
| S-5 | 3.16 uV | -97 dBm |
| S-6 | 6.3 uV | -91 dBm |
| S-7 | 12.6 uV | -85 dBm |
| S-8 | 25 uV | -79 dBm |
| S-9 | 50 uV | -73 dBm |
uV = microvolts across 50 ohms (signal voltage at the receiver's antenna connector)
P = E2 / R so P = 0.1 microvolts squared / 50 ohms
P = 2 x 10-16 or .0000000000000002 watts
Log10 ( 2 x 10-16 ) = -15.69897
-15.69897 x 10 = -156.9897 dBW
-156.9897 dBW -30 = -126.9897 = -127 dBm (good enough for the gals we go out with)
|
dBm to Microvolt conversion table (measured across 50 Ohms) dBm uV dBm uV dBm uV 0 224,000 -47 1,000 -94 4.47 -1 200,000 -48 891 -95 3.99 -2 178,000 -49 795 -96 3.55 -3 159,000 -50 709 -97 3.17 -4 141,000 -51 633 -98 2.82 -5 126,000 -52 563 -99 2.52 -6 112,000 -53 501 -100 2.24 -7 100,000 -54 447 -101 2.00 -8 89,100 -55 399 -102 1.78 -9 79,500 -56 355 -103 1.59 -10 70,900 -57 317 -104 1.41 -11 63,300 -58 282 -105 1.26 -12 56,300 -59 252 -106 1.12 -13 50,100 -60 224 -107 1.00 -14 44,700 -61 200 -108 0.891 -15 39,900 -62 178 -109 0.795 -16 35,500 -63 159 -110 0.709 -17 31,700 -64 141 -111 0.633 -18 28,200 -65 126 -112 0.563 -19 25,200 -66 112 -113 0.501 -20 22,400 -67 100 -114 0.447 -21 20,000 -68 89.1 -115 0.399 -22 17,800 -69 79.5 -116 0.355 -23 15,900 -70 70.9 -117 0.317 -24 14,100 -71 63.3 -118 0.282 -25 12,600 -72 56.3 -119 0.252 -26 11,200 -73 50.1 -120 0.224 -27 10,000 -74 44.7 -121 0.200 -28 8,900 -75 39.9 -122 0.178 -29 7,950 -76 35.5 -123 0.159 -30 7,090 -77 31.7 -124 0.141
dBm uV dBm uV dBm uV
-31 6,330 -78 28.2 -125 0.126 -32 5,630 -79 25.2 -126 0.112 -33 5,010 -80 22.4 -127 0.100 -34 4,470 -81 20.0 -128 0.0891 -35 3,990 -82 17.8 -129 0.0795 -36 3,550 -83 15.9 -130 0.0709 -37 3,170 -84 14.1 -131 0.0633 -38 2,820 -85 12.6 -132 0.0563 -39 2,520 -86 11.2 -133 0.0501 -40 2,240 -87 10.0 -134 0.0447 -41 2,000 -88 8.91 -135 0.0399 -42 1,780 -89 7.95 -136 0.0355 -43 1,590 -90 7.09 -137 0.0317 -44 1,410 -91 6.33 -138 0.0282 -45 1,260 -92 5.63 -139 0.0252 -46 1,120 -93 5.01 -140 0.0224
|
dBf
dBu
SINAD
Signal + noise / noise ratio
Transmitting:
The decibel as an absolute unit:
| dB uW | dBm | Power | dBW |
| 120 | 90 | 1 MW | 60 |
| 90 | 60 | 1 kW | 30 |
| 80 | 50 | 100 W | 20 |
| 70 | 40 | 10 W | 10 |
| 60 | 30 | 1 W | 0 |
| 50 | 20 | 100 mW | -10 |
| 40 | 10 | 10 mW | -20 |
| 33 | 3 | 2 mW | -27 |
| 32 | 2 | 1.58 mW | -28 |
| 31 | 1 | 1.26 mW | -29 |
| 30 | 0 | 1 mW | -30 |
Field intensity and power density:
uW / centimeter2 to uV / meter2 conversion
uV / meter2 to dBm conversion
Sometimes it is necessary to know the actual field intensity or power density at a given distance from a transmitter instead of the signal strength received by an antenna. Field intensity or power density calculations are necessary when estimating electromagnetic interference (EMI) effects, when determining potential radiation hazards, or in determining or verifying specifications.
Field intensity (field strength) is a general term that usually means the magnitude of the electric field vector, commonly expressed in volts per meter. At frequencies above 100 MHz, and particularly above one GHz, power density (PD) terminology is more often used than field strength.
Power density and field intensity are related by equation [1]:
1. PD = E2 / Zo = E2 / ( 120 ∙ pi ) = E2 / 377
where PD is in W/m2, E is the RMS value of the field in volts/meter and 377 ohms is the characteristic impedance of free space. When the units of PD are in mW/cm2, then PD (mW/cm2) = E2/3770.
Conversions between field strength and power density when the impedance is 377 ohms, can be obtained from Table 1. It should be noted that to convert dBm/m2 to dBV/m add 115.76 dB. Sample calculations for both field intensity and power density in the far field of a transmitting antenna are in the Power Density Section which follows.
Note that the "/" term before m, m2, and cm2 in Table 1 mean "per", i.e. dBm per m2, not to be confused with the division sign which is valid for the Table 1 equation P=E2/Zo. Remember that in order to obtain dBm from dBm/m2 given a certain area, you must add the logarithm of the area, not multiply. The values in the table are rounded to the nearest dBW, dBm, etc. per m2 so the results are less precise than a typical handheld calculator and may be up to a dB off.
Table 1. Conversion Table - Field
Intensity and Power Density PD = E2/Z0
(
Related by free space impedance = 377 ohms )
|
E |
20 log106 (E) (dBµV/m) |
PD (watts/m2) |
10 log
PD (dBW/m2) |
Watts/cm2 |
dBW/cm2 |
mW/cm2 |
dBm/cm2 |
dBm/m2 |
| 7,000 5,000 3,000 4,000 1,000 |
197 194 190 186 180 |
130,000 66,300 23,900 10,600 2,650 |
+51 +48 +44 +40 +34 |
13 6.6 2.4 1.1 .27 |
+11 +8 +4 0 -6 |
13,000 6,630 2,390 1,060 265 |
+41 +38 +34 +30 +24 |
+81 +78 +74 +70 +64 |
| 700 500 300 200 100 |
177 174 170 166 160 |
1,300 663 239 106 27 |
+31 +28 +24 +20 +14 |
.13 .066 .024 .011 .0027 |
-9 -12 -16 -20 -26 |
130 66 24 11 2.7 |
+21 +18 +14 +10 +4 |
+61 +58 +54 +50 +44 |
| 70 50 30 20 10 |
157 154 150 146 140 |
13 6.6 2.4 1.1 .27 |
+11 +8 +4 +0 -6 |
1.3x10-3 6.6x10-4 2.4x10-4 1.1x10-4 2.7x10-5 |
-29 -32 -36 -40 -46 |
1.3 .66 .24 .11 .027 |
+1 -2 -6 -10 -16 |
+41 +38 +34 +30 +24 |
| 7 5 3 2 1 |
137 134 130 126 120 |
.13 .066 .024 .011 .0027 |
-9 -12 -16 -20 -26 |
1.3x10-5 6.6x10-6 2.4x10-6 1.1x10-6 2.7x10-7 |
-49 -52 -56 -60 -66 |
.013 66x10-4 24x10-4 11x10-4 2.7x10-4 |
-19 -22 -26 -30 -36 |
+21 +18 +14 +10 +4 |
|
E |
20 log106 (E) (dBµV/m) |
PD (watts/m2) |
10 log
PD (dBW/m2) |
Watts/cm2 | dBW/cm2 | mW/cm2 | dBm/cm2 | dBm/m2 |
| 0.7 0.5 0.3 0.2 0.1 |
117 114 110 106 100 |
1.3x10-3 6.6x10-4 2.4x10-4 1.1x10-4 2.7x10-5 |
-29 -32 -36 -40 -46 |
1.3x10-7 6.6x10-8 2.4x10-8 1.1x10-8 2.7x10-9 |
-69 -72 -76 -80 -86 |
1.3x10-4 66x10-4 24x10-4 11x10-4 2.7x10-6 |
-39 -42 -46 -50 -56 |
+1 -2 -6 -10 -16 |
| 70x10-3 50x10-3 30x10-3 20x10-3 10x10-3 |
97 94 90 86 80 |
1.3x10-5 6.6x10-6 2.4x10-6 1.1x10-6 2.7x10-7 |
-49 -52 -56 -60 -66 |
1.3x10-9 6.6x10-10 2.4x10-10 1.1x10-10 2.7x10-11 |
-89 -92 -96 -100 -106 |
1.3x10-6 66x10-8 24x10-8 11x10-8 2.7x10-8 |
-59 -62 -66 -70 -76 |
-19 -22 -26 -30 -36 |
| 7x10-3 5x10-3 3x10-3 2x10-3 1x10-3 |
77 74 70 66 60 |
1.3x10-7 6.6x10-8 2.4x10-8 1.1x10-8 2.7x10-9 |
-69 -72 -76 -80 -86 |
1.3x10-11 6.6x10-12 2.4x10-12 1.1x10-12 2.7x10-13 |
-109 -112 -116 -120 -126 |
1.3x10-8 66x10-10 24x10-10 11x10-10 2.7x10-10 |
-79 -82 -86 -90 -96 |
-39 -42 -46 -50 -56 |
| E (Volts/m) |
20 log106 (E) (dBµV/m) |
PD (watts/m2) |
10 log
PD (dBW/m2) |
Watts/cm2 | dBW/cm2 | mW/cm2 | dBm/cm2 | dBm/m2 |
| 7x10-4 5x10-4 3x10-4 2x10-4 1x10-4 |
57 54 50 46 40 |
1.3x10-9 6.6x10-10 2.4x10-10 1.1x10-10 2.7x10-11 |
-89 -92 -96 -100 -106 |
1.3x10-13 6.6x10-14 2.4x10-14 1.1x10-14 2.7x10-15 |
-129 -132 -136 -140 -146 |
1.3x10-10 66x10-12 24x10-12 11x10-12 2.7x10-12 |
-99 -102 -106 -110 -116 |
-59 -62 -66 -70 -76 |
| 7x10-5 5x10-5 3x10-5 2x10-5 1x10-5 |
37 34 30 26 20 |
1.3x10-11 6.6x10-12 2.4x10-12 1.1x10-12 2.7x10-13 |
-109 -112 -116 -120 -126 |
1.3x10-15 6.6x10-16 2.4x10-16 1.1x10-16 2.7x10-17 |
-149 -152 -156 -160 -166 |
1.3x10-12 66x10-14 24x10-14 11x10-14 2.7x10-14 |
-119 -122 -126 -130 -136 |
-79 -82 -86 -90 -96 |
| 7x10-6 5x10-6 3x10-6 2x10-6 1x10-6 |
17 14 10 6 0 |
1.3x10-13 6.6x10-14 2.4x10-14 1.1x10-14 2.7x10-15 |
-129 -132 -136 -140 -146 |
1.3x10-17 6.6x10-18 2.4x10-18 1.1x10-18 2.7x10-19 |
-169 -172 -176 -180 -186 |
1.3x10-14 66x10-16 24x10-16 11x10-16 2.7x10-16 |
-139 -142 -146 -150 -156 |
-99 -102 -106 -110 -116 |
Numbers in table are rounded off
Voltage measurements
Coaxial cable typically has input impedances of 50, 75,
and 93
,
(nominal impedance) with 50 ohm being the most common. Other types of cabling
include 300 ohm and 450 ohm twinlead.
In the 50 ohm case, power and voltage are related by:
2. P = E2 / Zo = E2 / 50 = 50 ∙ I2
Conversions between measured power, voltage, and current where the typical impedance is 50 ohms can be obtained from Table 2. The dBµA current values are given because sometimes a current probe is used to determine the powerline input current to the system .
Matching cable impedance
In performing measurements, we must take into account an impedance mismatch between measurement devices (typically 50 ohms) and free space (377 ohms).
Field strength approach
To account for the impedance difference, the antenna factor (AF) is defined as: AF=E/V, where E is field intensity which can be expressed in terms taking 377 ohms into account and V is measured voltage which can be expressed in terms taking 50 ohms into account.
Power density approach
To account for the impedance difference , the antenna's effective capture area term, Ae relates free space power density PD with received power, Pr , i.e. Pr = PD Ae. Ae is a function of frequency and antenna gain and is related to AF
Examples:
Table 2. Conversion Table - Volts to Watts and dBµA
(Px = Vx2/Z - Related by line impedance of 50 ohms)
| Volts | dBV | dBµV | Watts | dBW | dBm | dBµA |
| 700 500 300 200 100 |
56.0 53.9 49.5 46.0 40.0 |
176.0 173.9 169.5 166.0 160.0 |
9800 5000 1800 800 200 |
39.9 37.0 32.5 29.0 23.0 |
69.9 67.0 62.5 59.0 53.0 |
142.9 140.0 135.5 132.0 126.0 |
| 70 50 30 20 10 |
36.9 34.0 29.5 26.0 20.0 |
156.9 154.0 149.5 146.0 140.0 |
98 50 18 8 2 |
19.9 17.0 12.5 9.0 3.0 |
49.9 47.0 42.5 39.0 33.0 |
122.9 120.0 115.5 112.0 106.0 |
| 7 5 3 2 1 |
16.9 14.0 9.5 6.0 0 |
136.9 134.0 129.5 126.0 120.0 |
0.8 0.5 0.18 0.08 0.02 |
0 -3.0 -7.4 -11.0 -17.0 |
29.9 27.0 22.5 19.0 13.0 |
102.9 100.0 95.6 92.0 86.0 |
| 0.7 0.5 0.3 0.2 0.1 |
-3.1 -6.0 -10.5 -14.0 -20.0 |
116.9 114.0 109.5 106.0 100.0 |
9.8 x 10-3 5.0 x 10-3 1.8 x 10-3 8.0 x 10-4 2.0 x 10-4 |
-20.1 -23.0 -27.4 -31.0 -37.0 |
9.9 7.0 2.6 -1.0 -7.0 |
82.9 80.0 75.6 72.0 66.0 |
| Volts | dBV | dBµV | Watts | dBW | dBm | dBµA |
| .07 .05 .03 .02 .01 |
-23.1 -26.0 -30.5 -34.0 -40.0 |
96.9 94.0 89.5 86.0 80.0 |
9.8 x 10-5 5.0 x 10-5 1.8 x 10-5 8.0 x 10-6 2.0 x 10-6 |
-40.1 -43.0 -47.4 -51.0 -57.0 |
-10.1 -13.0 -17.7 -21.0 -27.0 |
62.9 60.0 55.6 52.0 46.0 |
| 7 x 10-3 5 x 10-3 3 x 10-3 2 x 10-3 1 x 10-3 |
-43.1 -46.0 -50.5 -54.0 -60.0 |
76.9 74.0 69.5 66.0 60.0 |
9.8 x 10-7 5.0 x 10-7 1.8 x 10-7 8.0 x 10-8 2.0 x 10-8 |
-60.1 -63.0 -67.4 -71.0 -77.0 |
-30.1 -33.0 -37.4 -41.0 -47.0 |
42.9 40.0 35.6 32.0 26.0 |
| 7 x 10-4 5 x 10-4 3 x 10-4 2 x 10-4 1 x 10-4 |
-64.1 -66.0 -70.5 -74.0 -80.0 |
56.9 54.0 49.5 46.0 40.0 |
9.8 x 10-9 5.0 x 10-9 1.8 x 10-9 8.0 x 10-10 2.0 x 10-10 |
-80.1 -83.0 -87.4 -91.0 -97.0 |
-50.1 -53.0 -57.4 -61.0 -67.0 |
22.9 20.0 15.6 12.0 6.0 |
| 7 x 10-5 5 x 10-5 3 x 10-5 2 x 10-5 1 x 10-5 |
-84.1 -86.0 -90.5 -94.0 -100.0 |
36.9 34.0 29.5 26.0 20.0 |
9.8 x 10-11 5.0 x 10-11 1.8 x 10-11 8.0 x 10-12 2.0 x 10-12 |
-100.1 -103.0 -107.4 -111.0 -117.0 |
-70.1 -73.0 -77.4 -81.0 -87.0 |
2.9 0 -4.4 -8.0 -14.0 |
| Volts | dBV | dBµV | Watts | dBW | dBm | dBµA |
| 7 x 10-6 5 x 10-6 3 x 10-6 2 x 10-6 1 x 10-6 |
-104.1 -106.0 -110.5 -114.0 -120.0 |
16.9 14.0 9.5 6.0 0 |
9.8 x 10-13 5.0 x 10-13 1.8 x 10-13 8.0 x 10-14 2.0 x 10-14 |
-120.1 -123.0 -127.4 -131.0 -137.0 |
-90.1 -93.0 -97.4 -101.0 -107.0 |
-17.1 -20.0 -24.4 -28.0 -34.0 |
| 7 x 10-7 5 x 10-7 3 x 10-7 2 x 10-7 1 x 10-7 |
-124.1 -126.0 -130.5 -134.0 -140.0 |
-3.1 -6.0 -10.5 -14.0 -20.0 |
9.8 x 10-15 5.0 x 10-15 1.8 x 10-15 8.0 x 10-16 2.0 x 10-16 |
-140.1 -143.0 -147.4 -151.0 -157.0 |
-110.1 -113.0 -117.4 -121.0 -127.0 |
-37.1 -40.0 -44.4 -48.0 -54.0 |
Conversion Between Field Intensity (Table 1) and Power Received (Table 2).
Power received (watts or milliwatts) can be expressed in terms of field intensity (volts/meter or µv/meter) using equation [3]:
3. Power Received ( Pr ) = ( E2 / ( 480 ∙ pi2 )) ∙ ( c2 / f2 ) ∙ G
or in log form:
4. 10 log Pr = 20 log E + 10 log G - 20
log f + 10 log (c2/480
2)
Then
5. 10 log Pr = 20 log E1 + 10 log G - 20 log f1 + K4
Where K4 = 10 ∙ Log10 [( c2 / ( 480 ∙ pi2 )) ∙ ( Watts to mW ) / (( volts to uV )2 ∙ ( Hz to MHz or GHz )2 ) ]
| Values of K4 (dB) | ||||
| Pr | E1 | f1(Hz) | f1(MHz) | f1(GHz) |
| Watts (dBW) |
volts/meter | 132.8 | 12.8 | -47.2 |
| µv/meter | 12.8 | -107.2 | -167.2 | |
| mW (dBm) |
volts/meter | 162.8 | 42.8 | -17.2 |
| µv/meter | 42.8 | -77.2 | -137.7 | |
The derivation of equation [3] follows:
| Equation | Terms |
| PD= E2/120
|
(v2/ohm) |
| Ae =
|
(m2) |
| Pr = PDAe | (W/m2)(m2) |
| therefore: |
(v2/m2ohm)(m2) |
| (m/sec)(sec) | |
| therefore: |
(v2/m2ohm)(m2/sec2)(sec2) or v2/ohms = watts |
Bottom line here is to get close with the chart, use a little windage if necessary and call it good
Common types - yagi, quad, quagi
Special - loop, double parallelogram rhombic
The rhombic antenna:
When we think of the rhombic antenna or any other type of traveling wave antenna, we generally picture its use on the HF bands. These high gain wire arrays can also be used at VHF and UHF frequencies and because of the shorter wavelength, wire antennas can be constructed in a limited amount of space. At UHF frequencies a wire array can easily be made to rotate. The antenna featured here is a particularly long (for its design frequency) and high gain rhombic array called the Double parallelogram rhombic antenna or LaPorte rhombic. It is claimed to have a free space gain of 27 dBi and in the UHF band it can be constructed on a supporting frame about 24 feet in length and 12 feet wide. (full details will be given in the future)
Roughly estimating the (free space) gain of a yagi antenna when its active boom length is known.
The front to back ratio, swr bandwidth, and radiation resistance of a yagi antenna are dependent upon the number of elements used. Although gain is also effected, the primary factor in achieving gain is the length of the boom, from the reflector to the last director.
example: the KLM 2M-13LBA is a two meter 13 element yagi incorporating a dual driven element (for bandwidth) on a relatively long boom.
The boom length from the reflector to the last director is 21 feet 1 7/8 inches or close to 254 inches. One wavelength at 146 MHz is close to 81 inches.
254 / 81 = 3.1, multiply this by 10 and we now have 31, this is the power gain ratio, now convert it to a decibel, using the chart at the top of this page, we are real close to 15 dBi
This estimate is within a dB of KLM's advertised gain for the antenna.
The Uzkov limit defines the maximum gain theoretically possible for an array
of elements. The limit is 10.3 dBd for four dipole elements. This particular
antenna uses 4 driven dipole elements on a 0.6
boom the 4 elements are fed (from back to front) at 0°, -172°, 16°, and -156°
Frequency scaling using proportion
Changing the element diameter of a yagi design:
When a design for a home made beam is chosen from a cookbook the author rarely uses the exact material that the builder has a surplus of. The diameter of a yagi element has great influence upon the reactance of the element at the design frequency. Arbitrarily making seemingly small changes in element diameter can ruin the performance of an antenna. Changing the diameter of a 2 meter driven element from 3/8 inch to 5/32 inch will increase its overall length by 1 inch. The 35 inch element now has to be a hair over 36 inches in order for the element to have the same reactance at 144 MHz (in this case -79.52 ohms).
The process may seem involved at first but the math is quite simple, if you use windows calculator you will need a scratch pad to keep things in order, if you use an HP-48 go with the stack.
Formula 1 ( this will determine element reactance )
X = ((430.3 Log10 ( 2
/ D1 )) - 320) (( 2 L1 /
) - 1) + 40
D1 = original element diameter
L1 = original element length
= wavelength ( of design frequency = 300 / MHz ) in same units as
D1 and L1 ( m, mm, in )
Formula 2 ( this will determine the new element length )
L2 = (( X - 40 ) / (( 430.3 Log10 ( 2
/ D2 )) - 320) + 1 ) (
/ 2 )
X = element reactance ( determined in previous formula )
D2 = new element diameter
L2 = new element length
= wavelength (of design frequency = 300 / MHz ) in same units as
D2 ( m, mm, in )
Design frequency = 144 MHz
= 300 / 144 = 2.083 m = 2083 mm = 82.007 inches
L1 = 35 inches
D1 = 3/8 inches = .375 inches
Solve for X,
[1] 2
= 164.014
[2] 164.014 / D1 = 437.371
[3] Log10 437.371 = 2.641
[4] 2.641 • 430.3 = 1136.422
[5] 1136.422 - 320 = 816.422
[6] 2 • L1 = 70
[7] 70 /
= 0.8536
[8] 0.8536 -1 = -0.1464
[9] -0.1464 • 816.422 (answer from step 5) = -119.52
[10] -119.52 + 40 = -79.52 ohms (reactive)
X = -79.52 ohms
now plug X (the reactance of the original element) and D2 (the new diameter) back into the formula sideways and solve for L2 (the new length)
D2 = 5/32 = 0.15625
[11] 2
= 164.014
[12] 164.014 / D2 = 1049.69
[13] Log10 1049.69 = 3.02
[14] 3.02 • 430.3 = 1299.506
[15] 1299.506 - 320 = 979.506
[16] X - 40 = -119.52
[17] -119.52 / 979.506 (answer from step 15) = -0.12202
[18] -0.12202 + 1 = 0.878
[19]
/ 2 = 41.0035
[20] 41.0035 • 0.878 (answer from step 18) = 36.001 inches
Answer L2 = 36.001 inches
This process must be repeated for each element in which the diameter is changed
Example: 19.32458 inches
Drop the 19 and multiply the remaining decimal by the most accurate desired denominator
In this case we are shooting for 1/32 of an inch accuracy
0.32458 • 32 = 10.386
so we are looking at 10.386 32nds rounded to 10/32 and reduced to 5/16
19.32458 inches becomes 19 5/16 inches and is accurate within 1/32 of an inch
Example: 7/16" diameter
Multiply the denominator by 2
Radius = 7/32"
The effects of a conductive boom on element lengths:
The Boom Correction Factor
When modeling an antenna using highly developed computer algorithms, hundreds or even thousands of iterations later you have finally settled upon a yagi design that meets your needs. The only real problem is, that unless you use a non conductive boom such as fiberglass, all of your element lengths must be tweaked. This section will show you how to compensate for the effects of a conductive boom.
The method used to mount elements to a boom can affect antenna performance,
particularly for Yagi arrays at VHF and UHF. Through-the-boom mounting on a
conductive boom increases element effective diameter and raises the resonant
frequency of the element. To compensate for this, the element lengths must be
increased by a fraction of the boom diameter. This is referred to as the Boom
Correction Factor.
When constructing a Yagi antenna with a conductive boom, use this formula to increase the calculated element lengths.
C = (25.195*B) - (229*B^2)
The formula is valid for booms with diameters less than .055 wavelength. At 446 MHz, a 1.5 inch boom slightly exceeds this limit.
C is the correction factor expressed as a fraction of boom diameter B in wavelengths.
C is the correction factor for non-insulated through-the-boom element mounting.
The correction factor for insulated through-the-boom mounting is approximately 50% of C.
For example, a .01-wavelength diameter boom requires an element-length correction of 23% of the boom diameter.
A 0.01 Wavelength boom diameter at 446 MHz is only 6.73mm (slightly over 1/4 inch) the next example will reflect something more realistic.
Example 1:
Frequency = 446 MHz Wavelength = 673mm (300/446)
Boom is 1" aluminum = 25.4mm 25.4/673 = .038 Wavelength
C = (25.195 * .038) - (229 * (.038 * .038))
C = 0.957 - 0.33
C = 0.627 or 63%
0.63 * 25.4 = 15.92 = 16mm
In this example 16 millimeters must be added to the total length of each element for conductive through-the-boom mounting, If insulated through-the-boom mounting is employed, only 8 millimeters must be added to the total length of each element. Make certain that you do not misinterpret the total length of each element with the element half-length.
Conductivity of common metals
Effects of conductivity on skin effect and efficiency
Dielectric constant of various insulators
Lossy dielectric materials
Numeric Electromagnetic Code (NEC) and computerized antenna design
Array gain
Pattern gain
Height gain
Ground reflection
Polarization: vertical, horizontal, omni, circular
The polarization of the antennas for any two stations in communication is generally the same, either horizontal or vertical. In some instances circular polarization is employed. The polarization is generally consistent with the mode of operation and the frequency sub-band. This rule is not necessarily cast in stone so contradictions will eventually arise.
Cross-polarization may be illustrated as one station transmitting on a vertically polarized antenna and the other receiving on a horizontally polarized antenna. Rule of thumb in this case is said to be 20 to 25 dB of loss due to 90 degree cross-polarization. This figure was obtained by experimentation but is not a truly accurate figure.
There is a formula which will give a "worst case" figure for this loss, by worst case we mean two antennas in free space, or more realistically in an RF Anechoic chamber, eliminating multipath reflections.
The formula (as entered into the HP-48) is: Loss = ( 10 * Log10 ( sq ( Cos ( Theta ) ) ) )
Loss = dB
Theta = The angle of displacement (between two antennas in communication)
Example 1, one antenna is vertically polarized and the other is at a 45 degree angle: (work the formula backwards)
Theta = 45 degrees
Cos Theta = 0.707
Square of Cos Theta = 0.5
Log10 of 0.5 = -0.3010
10 x -0.3010 = - 3.010
Loss = 3 dB
Example 2, one antenna is vertically polarized and the other is horizontally polarized:
Theta = 89 degrees ( We will fudge by one degree here because the Cosine of 90 degrees is 0, which causes heartburn with digital apparatus)
Cos Theta = 0.0174
Square of Cos Theta = 0.0003045
Log10 of 0.0003045 = -3.516
10 x -3.516 = - 35.16
Loss = 35 dB
Simple Cross-polarization chart:
For argument's sake, presume 90 to be vertical and 0 to be horizontal. 45 is a 2 meter mobile whip on a vehicle at highway speeds.
RHCP = right hand circular polarization.
LHCP = left hand circular polarization.
AX = axial also called linear polarization where both horizontal and vertical elements are fed in-phase.
|
Antenna 1 |
Antenna 2 |
Loss in dB |
|
90 |
90 |
0 |
|
90 |
0 |
25 to 40 |
|
90 |
45 |
3 |
|
RHCP |
0 |
3 |
|
RHCP |
90 |
3 |
|
RHCP |
LHCP |
25 to 40 |
|
AX |
90 |
3 |
| AX | 0 | 3 |
| AX | LHCP | 3 |
|
AX |
RHCP |
3 |
Phasing harness for the Cushcraft A148-20T
Parts needed:
A few feet of RG-8X Belden or equivalent 50 ohm coaxial cable.
A few feet of RG-6 type low loss 75 ohm coaxial cable. I prefer Belden 9248
because it has a tinned copper braid as opposed to the aluminum braid used in
most RG-6 cable, also the center conductor is #18 solid copper opposed to copper
coated steel which I avoid for reasons that are out of the scope of this
article.
1 UHF Tee connector
1 UHF double female coupler
6 PL-259 connectors. Use silver/Teflon or silver/ceramic not the phenolic cheapies
available at Radio Shack and other places. Phenolic is very lossy at VHF
frequencies
6 UG-176 adapters
Description:
There are two parts to this harness, the phasing lines and the delay line.
Construction:
you will need to cut 3 pieces of coax, each will be 1/4 wavelength at the design
frequency (times the velocity factor of the cable). 1/4 wave sections have a
relatively low Q so the center of the two meter band was chosen. The lengths are
not critical (within a quarter of an inch is ok)
For the two 75 ohm pieces;
(234/146) x 12 = 19.23 inches, the velocity factor for 9248 Belden is around 78%
or .78 so 19.23 inches x .78 = about 15 inches
For the one 50 ohm piece;
(234/146) x 12 = 19.23 inches, the velocity factor for RG-8X Belden is around
75% or .76, so19.23 inches x .76 = about 14.6 (14 1/2) inches
Assembly: See diagram below
Changing polarization:
The illustration will yield RHCP or right hand circular polarization which is
pretty much the standard. This can be changed if necessary however...
RHCP = delay line connected to the horizontal driven element.
LHCP = delay line connected to vertical driven element.
Axial Polarization, also called linear polarization = no delay line Just the 75 ohm phasing harness.
Both sets of elements are fired at the same time, there is a loss of 3 db when
talking to a vertical , horizontal or circularly polarized station.
These rules apply only to dual polarity beams which have the Horizontal and Vertical elements at the same spacing, some manufacturers 'stagger' the horizontal and vertical bays (like KLM) then things become very different

Effects of the mast (and feedline) on antenna performance (E plane distortion)
Pattern effects from stacking
Feeding stacked arrays
Coaxial phasing harnesses, impedance matching tricks
Power dividers
Baluns: 1/4 wave sleeve
Feed lines
Types of coaxial cables
Coax loss chart
Contamination
Water
Minimum radius
Avoid using tie wraps to secure coaxial cable to tower legs etc. The constant pressure will cause the coax to become pinched at each tie wrap. This in turn will create an impedance-bump at each tie wrap, increasing overall cable losses and degrading the noise figure of the system. I generally use good old Scotch 33 black electrical tape which is wider and spreads out the pressure as well as being flexible so it does not "dent" the coaxial cable over time. As an added bonus it eventually makes a black sticky mess on the coax, but does not effect the system electrically. When wrapping the tape do not stretch it too tightly, use a scissors or knife to cut the tape rather than stretching it until it breaks. This will reduce the number of tiny black flags flapping in the wind.
Always unroll coaxial cable, as if reeling out thread from a spool. Uncoiling (like stretching a spring) will cause repeated twists in the cable, creating small but cumulative losses.
Combine uncoiling with tie wraps and with a bit of luck you won't hear anything.
Propagation
Path loss
Free space
Radio path horizon
Tropospheric ducting
Aurora
Meteor scatter
Backscatter
Lightning
Station capabilities (putting it all together)
Summing gains and losses (Link budget analysis)
Estimating station to station range and signal quality
The Passive Transfer of RF energy (Smoke and Mirrors, aka the repeater extender project)
Interference
Bibliography