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Yashwanth RCS Reduction 1
Contents
Introduction
Reduction
Methods of reduction
 Purpose shaping
 Active Cancellation
 Radar absorbent material
 Plasma based RCS reduction
 Optimization methods
RCS of antenna
Advantages and Disadvantages
Conclusion and scope
References
Yashwanth RCS Reduction 2
Brief Intro
• Radar cross-section (RCS) is a measure of how detectable an object is with a
radar. A larger RCS indicates that an object is more easily detected.
• An object reflects a limited amount of radar energy back to the source. The
factors that influence this include:
• The material of which the target is made;
• The absolute size of the target;
• The relative size of the target (in relation to the wavelength of the illuminating
illuminating radar);
• The incident angle (angle at which the radar beam hits a particular portion of
of target which depends upon shape of target and its orientation to the radar
radar source);
• The reflected angle (angle at which the reflected beam leaves the part of the
the target hit, it depends upon incident angle);
• The polarization of transmitted and the received radiation in respect to the
orientation of the target Yashwanth RCS Reduction 3
Reduction
• RCS reduction is chiefly important in stealth technology for aircraft, missiles, ships, and other military
vehicles. With smaller RCS, vehicles can better evade radar detection, whether it be from land-based
installations, guided weapons or other vehicles. Reduced signature design also improves platforms'
overall survivability through the improved effectiveness of its radar counter-measures.
• Several methods exist. The distance at which a target can be detected for a given radar configuration
varies with the fourth root of its RCS.Therefore, in order to cut the detection distance to one tenth, the
RCS should be reduced by a factor of 10,000. Whilst this degree of improvement is challenging, it is
often possible when influencing platforms during the concept/design stage and using experts and
advanced computer code simulations to implement the control options
Yashwanth RCS Reduction 4
Methods of Reduction
• Purpose Shaping
• Active Cancellation
• Radar absorbent material
• Plasma based RCS reduction
• Optimization methods
Yashwanth RCS Reduction 5
Purpose Shaping
• With purpose shaping, the shape of the target’s reflecting surfaces is designed such that they reflect
energy away from the source. The aim is usually to create a “cone-of-silence” about the target’s direction
of motion. Due to the energy reflection, this method is defeated by using Passive (multistatic) radars.
• Purpose-shaping can be seen in the design of surface faceting on the F-117A Nighthawk stealth fighter.
This aircraft, designed in the late 1970s though only revealed to the public in 1988, uses a multitude of
flat surfaces to reflect incident radar energy away from the source.
• Yue suggests that limited available computing power for the design phase kept the number of surfaces to
a minimum. The B-2 Spirit stealth bomber benefited from increased computing power, enabling its
contoured shapes and further reduction in RCS. The F-22 Raptor and F-35 Lightning II continue the
trend in purpose shaping and promise to have even smaller monostatic RCS.
Yashwanth RCS Reduction 6
Active Cancellation
• With active cancellation, the target generates a radar signal equal in intensity but opposite in phase to the
predicted reflection of an incident radar signal (similarly to noise canceling ear phones).
• This creates destructive interference between the reflected and generated signals, resulting in reduced
RCS. To incorporate active cancellation techniques, the precise characteristics of the waveform and angle
of arrival of the illuminating radar signal must be known, since they define the nature of generated
energy required for cancellation.
• Except against simple or low frequency radar systems, the implementation of active cancellation
techniques is extremely difficult due to the complex processing requirements and the difficulty of
predicting the exact nature of the reflected radar signal over a broad aspect of an aircraft, missile or other
target
Yashwanth RCS Reduction 7
Radar absorbent material
• Radar absorbent material (RAM) can be used in the original construction, or as an addition to highly
reflective surfaces. There are at least three types of RAM: resonant, non-resonant magnetic and non-
resonant large volume.
• Resonant but somewhat 'lossy' materials are applied to the reflecting surfaces of the target. The
incident radar energy is reflected from the outside and inside surfaces of the RAM to create a
destructive wave interference pattern.
• Non-resonant magnetic RAM uses ferrite particles suspended in epoxy or paint to reduce the
reflectivity of the surface to incident radar waves.
• Large volume RAM is usually resistive carbon loading added to fiberglass hexagonal cell aircraft
structures or other non-conducting components.
Yashwanth RCS Reduction 8
Plasma based RCS reduction
• Plasma stealth is a proposed process to use ionized gas (plasma) to reduce the RCS of an aircraft.
Interactions between electromagnetic radiation and ionized gas have been extensively studied for many
purposes, including concealing aircraft from radar as stealth technology.
• Various methods might plausibly be able to form a layer or cloud of plasma around a vehicle to deflect or
absorb radar, from simpler electrostatic or radio frequency (RF) discharges to more complex laser
discharges. It is theoretically possible to reduce RCS in this way, but it may be very difficult to do so in
practice.
Yashwanth RCS Reduction 9
Optimization methods
• Thin non-resonant or broad resonance coatings can be modeled with a Leontovich impedance boundary
condition (see also Electrical impedance). This is the ratio of the tangential electric field to the tangential
magnetic field on the surface, and ignores fields propagating along the surface within the coating. For an
isotropic surface the ideal surface impedance is equal to the 377 ohm impedance of free space.
• To calculate the radar cross-section of such a stealth body, one would typically do one-dimensional
reflection calculations to calculate the surface impedance, then two dimensional numerical calculations
to calculate the diffraction coefficients of edges and small three dimensional calculations to calculate the
diffraction coefficients of corners and points.
• Optimization is in the reverse order. First one does high frequency calculations to optimize the shape and
find the most important features, then small calculations to find the best surface impedances in the
problem areas, then reflection calculations to design coatings.
Yashwanth RCS Reduction 10
RCS of antenna
• For the case of an antenna the total RCS can be divided into two separate components as Structural Mode
RCS and Antenna Mode RCS. The two components of the RCS relates to the two scattering phenomena
that takes place at the antenna.
• When an electromagnetic signal falls on an antenna surface, some part of the electromagnetic energy is
scattered back to the space. This is called structural mode scattering.
• The remaining part of the energy is absorbed due to the antenna effect. Some part of the absorbed energy
is again scattered back into the space due to the impedance mismatches, called antenna mode scattering.
Yashwanth RCS Reduction 11
Advantages Disadvantages
• Survival of stealth vehicle
• Attacking is a benefit by this
process
• Invincible to the RADARs by
avoiding the damage of
counterfeits
• RADAR’s of multiple types can
easily detect the stealth
• Not easy to implement
• Optimized by boundary
conditions
• Difficult to expect and identify
the properties of the waves of
RADAR
Yashwanth RCS Reduction 12
Conclusion and Scope
 This Radar Cross section reduction is mostly useful
in the times of wars and as it is very difficult to
implement there are less number of vehicles which
are made of stealth technology
 Effective measures of RADARs has always been a
work in the research industries like
DRDO,ECIL,BEL etc,.
 RADAR technology must be improved in our country
in our fighter jets to improve defence skills so that
defeating the F-15 fighter jets of Pakistan can much
easier
 Development in Electronics and Communication
department is necessary for our country
Yashwanth RCS Reduction 13
References
• Skolnick, M.I., Introduction to Radar Systems, McGraw-Hill, 1980.
• Knott, Eugene; Shaeffer, John; Tuley, Michael (1993). Radar Cross
Section, 2nd ed. Artech House, Inc. p. 231. ISBN 0-89006-618-3.
• F-22 Raptor Stealth GlobalSecurity.org
• Bill Sweetman, Unconventional Weapon: What we learned about
stealth technology from the combat career of the F-117,
Smithsonian Air & Space Magazine, 01 January 2008
• Radar Cross Section Measurements (8-12 GHz)
• Ship RCS Table
• www.radartutorial.eu (Effektive Rückstrahlfläche (RCS); German)
• M. Skolnik: Introduction to radar systems. 2nd Edition, McGraw-
Hill, Inc., 1980, p. 44
• C.A., Advanced Engineering Electromagnetics, John Wiley & Sons,
1989. Yashwanth RCS Reduction 14
Yashwanth RCS Reduction 15

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Radar Cross Section Reduction

  • 2. Contents Introduction Reduction Methods of reduction  Purpose shaping  Active Cancellation  Radar absorbent material  Plasma based RCS reduction  Optimization methods RCS of antenna Advantages and Disadvantages Conclusion and scope References Yashwanth RCS Reduction 2
  • 3. Brief Intro • Radar cross-section (RCS) is a measure of how detectable an object is with a radar. A larger RCS indicates that an object is more easily detected. • An object reflects a limited amount of radar energy back to the source. The factors that influence this include: • The material of which the target is made; • The absolute size of the target; • The relative size of the target (in relation to the wavelength of the illuminating illuminating radar); • The incident angle (angle at which the radar beam hits a particular portion of of target which depends upon shape of target and its orientation to the radar radar source); • The reflected angle (angle at which the reflected beam leaves the part of the the target hit, it depends upon incident angle); • The polarization of transmitted and the received radiation in respect to the orientation of the target Yashwanth RCS Reduction 3
  • 4. Reduction • RCS reduction is chiefly important in stealth technology for aircraft, missiles, ships, and other military vehicles. With smaller RCS, vehicles can better evade radar detection, whether it be from land-based installations, guided weapons or other vehicles. Reduced signature design also improves platforms' overall survivability through the improved effectiveness of its radar counter-measures. • Several methods exist. The distance at which a target can be detected for a given radar configuration varies with the fourth root of its RCS.Therefore, in order to cut the detection distance to one tenth, the RCS should be reduced by a factor of 10,000. Whilst this degree of improvement is challenging, it is often possible when influencing platforms during the concept/design stage and using experts and advanced computer code simulations to implement the control options Yashwanth RCS Reduction 4
  • 5. Methods of Reduction • Purpose Shaping • Active Cancellation • Radar absorbent material • Plasma based RCS reduction • Optimization methods Yashwanth RCS Reduction 5
  • 6. Purpose Shaping • With purpose shaping, the shape of the target’s reflecting surfaces is designed such that they reflect energy away from the source. The aim is usually to create a “cone-of-silence” about the target’s direction of motion. Due to the energy reflection, this method is defeated by using Passive (multistatic) radars. • Purpose-shaping can be seen in the design of surface faceting on the F-117A Nighthawk stealth fighter. This aircraft, designed in the late 1970s though only revealed to the public in 1988, uses a multitude of flat surfaces to reflect incident radar energy away from the source. • Yue suggests that limited available computing power for the design phase kept the number of surfaces to a minimum. The B-2 Spirit stealth bomber benefited from increased computing power, enabling its contoured shapes and further reduction in RCS. The F-22 Raptor and F-35 Lightning II continue the trend in purpose shaping and promise to have even smaller monostatic RCS. Yashwanth RCS Reduction 6
  • 7. Active Cancellation • With active cancellation, the target generates a radar signal equal in intensity but opposite in phase to the predicted reflection of an incident radar signal (similarly to noise canceling ear phones). • This creates destructive interference between the reflected and generated signals, resulting in reduced RCS. To incorporate active cancellation techniques, the precise characteristics of the waveform and angle of arrival of the illuminating radar signal must be known, since they define the nature of generated energy required for cancellation. • Except against simple or low frequency radar systems, the implementation of active cancellation techniques is extremely difficult due to the complex processing requirements and the difficulty of predicting the exact nature of the reflected radar signal over a broad aspect of an aircraft, missile or other target Yashwanth RCS Reduction 7
  • 8. Radar absorbent material • Radar absorbent material (RAM) can be used in the original construction, or as an addition to highly reflective surfaces. There are at least three types of RAM: resonant, non-resonant magnetic and non- resonant large volume. • Resonant but somewhat 'lossy' materials are applied to the reflecting surfaces of the target. The incident radar energy is reflected from the outside and inside surfaces of the RAM to create a destructive wave interference pattern. • Non-resonant magnetic RAM uses ferrite particles suspended in epoxy or paint to reduce the reflectivity of the surface to incident radar waves. • Large volume RAM is usually resistive carbon loading added to fiberglass hexagonal cell aircraft structures or other non-conducting components. Yashwanth RCS Reduction 8
  • 9. Plasma based RCS reduction • Plasma stealth is a proposed process to use ionized gas (plasma) to reduce the RCS of an aircraft. Interactions between electromagnetic radiation and ionized gas have been extensively studied for many purposes, including concealing aircraft from radar as stealth technology. • Various methods might plausibly be able to form a layer or cloud of plasma around a vehicle to deflect or absorb radar, from simpler electrostatic or radio frequency (RF) discharges to more complex laser discharges. It is theoretically possible to reduce RCS in this way, but it may be very difficult to do so in practice. Yashwanth RCS Reduction 9
  • 10. Optimization methods • Thin non-resonant or broad resonance coatings can be modeled with a Leontovich impedance boundary condition (see also Electrical impedance). This is the ratio of the tangential electric field to the tangential magnetic field on the surface, and ignores fields propagating along the surface within the coating. For an isotropic surface the ideal surface impedance is equal to the 377 ohm impedance of free space. • To calculate the radar cross-section of such a stealth body, one would typically do one-dimensional reflection calculations to calculate the surface impedance, then two dimensional numerical calculations to calculate the diffraction coefficients of edges and small three dimensional calculations to calculate the diffraction coefficients of corners and points. • Optimization is in the reverse order. First one does high frequency calculations to optimize the shape and find the most important features, then small calculations to find the best surface impedances in the problem areas, then reflection calculations to design coatings. Yashwanth RCS Reduction 10
  • 11. RCS of antenna • For the case of an antenna the total RCS can be divided into two separate components as Structural Mode RCS and Antenna Mode RCS. The two components of the RCS relates to the two scattering phenomena that takes place at the antenna. • When an electromagnetic signal falls on an antenna surface, some part of the electromagnetic energy is scattered back to the space. This is called structural mode scattering. • The remaining part of the energy is absorbed due to the antenna effect. Some part of the absorbed energy is again scattered back into the space due to the impedance mismatches, called antenna mode scattering. Yashwanth RCS Reduction 11
  • 12. Advantages Disadvantages • Survival of stealth vehicle • Attacking is a benefit by this process • Invincible to the RADARs by avoiding the damage of counterfeits • RADAR’s of multiple types can easily detect the stealth • Not easy to implement • Optimized by boundary conditions • Difficult to expect and identify the properties of the waves of RADAR Yashwanth RCS Reduction 12
  • 13. Conclusion and Scope  This Radar Cross section reduction is mostly useful in the times of wars and as it is very difficult to implement there are less number of vehicles which are made of stealth technology  Effective measures of RADARs has always been a work in the research industries like DRDO,ECIL,BEL etc,.  RADAR technology must be improved in our country in our fighter jets to improve defence skills so that defeating the F-15 fighter jets of Pakistan can much easier  Development in Electronics and Communication department is necessary for our country Yashwanth RCS Reduction 13
  • 14. References • Skolnick, M.I., Introduction to Radar Systems, McGraw-Hill, 1980. • Knott, Eugene; Shaeffer, John; Tuley, Michael (1993). Radar Cross Section, 2nd ed. Artech House, Inc. p. 231. ISBN 0-89006-618-3. • F-22 Raptor Stealth GlobalSecurity.org • Bill Sweetman, Unconventional Weapon: What we learned about stealth technology from the combat career of the F-117, Smithsonian Air & Space Magazine, 01 January 2008 • Radar Cross Section Measurements (8-12 GHz) • Ship RCS Table • www.radartutorial.eu (Effektive Rückstrahlfläche (RCS); German) • M. Skolnik: Introduction to radar systems. 2nd Edition, McGraw- Hill, Inc., 1980, p. 44 • C.A., Advanced Engineering Electromagnetics, John Wiley & Sons, 1989. Yashwanth RCS Reduction 14