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ONEWAY RADAR EQUATION / RF PROPAGATION
The oneway (transmitter to receiver) radar equation is derived in this section. This equation is most
commonly used in RWR or ESM type of applications. The following is a summary of the important equations explored
in this section:
Recall
from Section 42 that the power density at a distant point from a radar with an antenna gain of G_{t} is
the power density from an isotropic antenna multiplied by the radar antenna gain.
Power density from radar,
[1]
If you could cover the entire spherical segment with your receiving antenna you would theoretically
capture all of the transmitted energy. You can't do this because no antenna is large enough. (A two degree segment
would be about a mile and threequarters across at fifty miles from the transmitter.)
A receiving antenna
captures a portion of this power determined by it's effective capture Area (A_{e}). The received power
available at the antenna terminals is the power density times the effective capture area (A_{e}) of the
receiving antenna.
For a given receiver antenna size the capture area is constant no matter how far it is from the transmitter,
as illustrated in Figure 1. This concept is shown in the following equation:
which is known as the oneway
(beacon) equation [2]
In order to maximize energy transfer between an antenna and transmitter or receiver, the antenna size should
correlate λ/4. Control of beamwidth shape may become a problem when the size of the active element exceeds several
wavelengths.
The
relation between an antenna's effective capture area (A_{e}) is:
Antenna Gain,
[3]
or: Equivalent Area, Ae =
[4]
effective aperture is in units of length squared, s proportional to wavelength. This physically means
that to maintain the gain when doubling the frequency, the area is reduced by 1/4. This concept is illustrated in
Figure 2.
If equation [4] is substituted into equation [2], the following relationship results:
Peak Power at Receiver Input = S (or P_{R}) =
[5]
is the signal calculated oneway from a transmitter to a receiver. For instance, a radar application might
be to determine the signal received by a RWR, ESM, or an ELINT receiver. It is a general purpose equation and
could be The free space travel of radio waves can, of course, be blocked, reflected, or distorted by objects in
their path such
As
received signal power decreases by 1/4 (6 dB). This is due to the R^{2} term in equation [5]. It
illustrates a square on radius is decreased by 1/2, you further blow up the balloon, so the diameter or radius is
doubled, the square has quadrupled in area.
The oneway free space loss factor (α_{1}),
(sometimes called the path loss factor) is given by the term 4πR^{2})(4π/λ^{2})
or (4πR /λ)2. As shown in Figure 3, the loss is due to the ratio of two factors (1)
the effective radiated area of the transmit antenna, which is the surface area of a sphere (4πR^{2})
at that distance (R), and (2) the effective capture
area
(A_{e}) of the receive antenna which has a gain of one. If a receiving antenna could capture the whole
surface area of the sphere, there would be no spreading loss, but a practical antenna will capture only a small
part of the spherical radiation. Space loss is calculated using isotropic antennas for both transmit and receive,
so
α_{1} is independent of the actual antenna. Using G_{r} = 1 in
equation [11] in section 31, A_{e} = λ/4π. Since this term is in the
denominator of α_{1}, the higher the frequency (lower λ) the more the space
loss. Since G_{t} and G_{r} are part of the oneway radar equation, S (or P_{r}) is
adjusted according to actual antennas as shown in the last portion of Figure 3. The value of the received signal
(S) is:
[6]
To convert this equation to dB form, it is
rewritten as:
( keep λ and R in same units)
[7]
Since λ = c / f, equation [7] can be rewritten as:
10 Log (S or P_{r}) = 10 Log(P_{t}G_{t}G_{r}) 
α_{1}
[8]
Where the oneway free space loss, α_{1}, is defined as:
* [9]
The signal received equation in dB form
is: 10log (Pr or S) = 10 log P_{t} + 10 log G_{t} + 10 log G_{r}
 α_{1} [10]
The oneway free space loss,
α_{1}, can be given in terms of a variable and constant term as follows:
[11]
The value of f_{1} can be either in MHz or GHz as shown with commonly used units of R in
the adjoining table.
Note: To avoid having to include additional terms for these calculations, always combine any transmission line
loss with antenna gain.
A value for the oneway free space loss (α_{1})
can be obtained from:
(a) The Oneway Free Space Loss graph (Figure 4). Added accuracy can be obtained
using the Frequency Extrapolation graph (Figure 5)
(b) The space loss nomograph (Figure 6 or 7)
(c) The formula for
α_{1}, equation [11].
FOR EXAMPLE:
Find the
value of the oneway free space loss, α_{1}, for an RF of 7.5 GHz at 100 NM.
(a) From Figure 4, find 100 NM on the Xaxis and estimate where 7.5 GHz is located between the 1
and 10 GHz lines (note dot). Read
α_{1} as 155 dB. An alternate way would be to read the
α_{1} at 1 GHz (138 dB) and add the frequency extrapolation value
(17.5 dB for 7.5:1, dot on Figure 5) to obtain the same 155 dB value.
(b) From the
nomogram (Figure 6), the value of
α_{1} can be read as 155 dB (Note the dashed line).
(c) From the
equation 11, the precise value of α_{1} is 155.3 dB.
Remember, α_{1} is a free space value. If there is atmospheric attenuation
because of absorption of RF due to certain molecules in the atmosphere or weather conditions etc., the atmospheric
attenuation is in addition to the space loss (refer to Section 51).
Figure 4. OneWay Free Space Loss
Figure 5. Frequency Extrapolation
Figure 6. OneWay Space Loss Nomograph For Distances Greater Than 10 Nautical Miles
Figure 7. OneWay Space Loss Nomograph For Distances Less Than 10 Nautical Miles
Figure 8. Visualization of OneWay Radar Equation
RWR/ESM RANGE EQUATION (OneWay)
The oneway radar (signal
strength) equation [5] is rearranged to calculate the maximum range R_{max} of RWR/ESM receivers. It
occurs when the received radar signal just equals S_{min} as follows:
[12]
In log form:
20 log R_{max} = 10 log P_{t} + 10 log G_{t}  10 log S_{min}
 20 log f + 20 log(c/4π) [13]
and since K_{1} = 20 log{4π/c times conversion units if not in m/sec,
m, and Hz} (Refer to section 43 for values of K1).
10 log R_{max} = ½[10 log P_{t} + 10
log G_{t}  10 log S_{min}  20 log f  K_{1}] ( keep P_{t}
and S_{min} in same units) [14]
If you want to convert back
from dB, then Rmax � , where M dB is the resulting number in the brackets of equation 14.
From Section 52,
Receiver Sensitivity / Noise, Smin is related to the noise factor S: S_{min}
= (S/N)_{min} (NF)KT_{o}B [15]
The oneway RWR/ESM range equation becomes:
[16]
RWR/ESM RANGE INCREASE AS A RESULT OF A SENSITIVITY INCREASE
As shown in equation [12] S_{min}^{1} proportional to R_{max}.
Therefore,
10 log S_{min} proportional to 20 log R_{max} and the table below results:
% Range Increase: Range + (% Range Increase) x Range = New Range
i.e., for a 6
dB sensitivity increase, 500 miles +100% x 500 miles = 1,000 miles
Range Multiplier:
Range x Range Multiplier = New Range i.e., for a 6 dB sensitivity increase
500 miles x 2 = 1,000 miles
RWR/ESM RANGE DECREASE AS A RESULT OF A SENSITIVITY DECREASE
As shown
in equation [12] S_{min} proportional to R_{max}.
Therefore, 10 log S_{min}
proportional to 20 log R_{max} and the table below results:
% Range Decrease:
Range  (% Range decrease) x Range = New Range
i.e., for a 6 dB sensitivity decrease, 500 miles  50% x 500
miles = 250 miles
Range Multiplier: Range x Range Multiplier = New Range i.e.,
for a 6 dB sensitivity decrease
500 miles x .5 = 250 miles
Example of OneWay Signal Strength: A 5 (or 7) GHz radar has a 70 dBm
signal fed through a 5 dB loss transmission line to an antenna that has 45 dB gain. An aircraft that is flying
31 km from the radar has an aft EW antenna with 1 dB gain and a 5 dB line loss to the EW receiver (assume all
antenna polarizations are the same).
Note: The respective transmission line losses will be combined with
antenna gains, i.e.:
5 +45 = 40 dB, 5  1 = 6 dB, 10 + 5 = 5 dB.
(1) What is the power level at the input of the EW receiver?
Answer (1): P_{r} at the input to
the EW receiver = Transmitter power  xmt cable loss + xmt antenna gain  space loss + rcvr antenna gain  rcvr
cable loss.
Space loss (from section 43) @ 5 GHz = 20 log f R + K1 = 20 log (5x31) + 92.44 = 136.25 dB.
Therefore, P_{r} = 70 + 40  136.25  6 = 32.25 dBm @ 5 GHz (P_{r} = 35.17 dBm @ 7 GHz since
α_{1} = 139.17 dB) (2) If the received signal is fed to a jammer with a
gain of 60 dB, feeding a 10 dB loss transmission line which is connected to an antenna with 5 dB gain, what is the
power level from the jammer at the input to the receiver of the 5 (or 7) GHz radar?
Answer (2): P_{r}
at the input to the radar receiver = Power at the input to the EW receiver+ Jammer gain  jammer cable loss +
jammer antenna gain  space loss + radar rcvr antenna gain  radar rcvr cable loss .
Therefore, P_{r}
= 32.25 + 60  5  136.25 + 40 = 73.5 dBm @ 5 GHz. (P_{r} = 79.34 dBm @ 7 GHz since
α_{1}
= 139.17 dB and Pt = 35.17 dBm).
This problem continues in section 44, 47, and 410.
Table of Contents
for Electronics Warfare and Radar Engineering Handbook
Introduction 
Abbreviations  Decibel  Duty
Cycle  Doppler Shift  Radar Horizon / Line
of Sight  Propagation Time / Resolution  Modulation
 Transforms / Wavelets  Antenna Introduction
/ Basics  Polarization  Radiation Patterns 
Frequency / Phase Effects of Antennas 
Antenna Near Field  Radiation Hazards 
Power Density  OneWay Radar Equation / RF Propagation
 TwoWay Radar Equation (Monostatic) 
Alternate TwoWay Radar Equation 
TwoWay Radar Equation (Bistatic) 
Jamming to Signal (J/S) Ratio  Constant Power [Saturated] Jamming
 Support Jamming  Radar Cross Section (RCS) 
Emission Control (EMCON)  RF Atmospheric
Absorption / Ducting  Receiver Sensitivity / Noise 
Receiver Types and Characteristics 
General Radar Display Types 
IFF  Identification  Friend or Foe  Receiver
Tests  Signal Sorting Methods and Direction Finding 
Voltage Standing Wave Ratio (VSWR) / Reflection Coefficient / Return
Loss / Mismatch Loss  Microwave Coaxial Connectors 
Power Dividers/Combiner and Directional Couplers 
Attenuators / Filters / DC Blocks 
Terminations / Dummy Loads  Circulators
and Diplexers  Mixers and Frequency Discriminators 
Detectors  Microwave Measurements 
Microwave Waveguides and Coaxial Cable 
ElectroOptics  Laser Safety 
Mach Number and Airspeed vs. Altitude Mach Number 
EMP/ Aircraft Dimensions  Data Busses  RS232 Interface
 RS422 Balanced Voltage Interface  RS485 Interface 
IEEE488 Interface Bus (HPIB/GPIB)  MILSTD1553 &
1773 Data Bus  This HTML version may be printed but not reproduced on websites.
