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{{Short description|Proposed aircraft stealth technology}}
'''Plasma stealth''' is a proposed process to use ionized gas ([[plasma (physics)|plasma]]) to reduce the [[radar cross-section]] (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.<ref name="laserplasma">{{cite conference
 
| author=I.V. Adamovich
'''Plasma stealth''' is a proposed process to use ionized gas ([[plasma (physics)|plasma]]) to reduce the [[radar cross-section]] (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.<ref name="laserplasma">{{cite conference
| author2=J. W. Rich
| author = I.V. Adamovich
| author3=A.P. Chernukho
| author2 = J. W. Rich
| author4=S.A. Zhdanok
| author3 = A.P. Chernukho
| title=Analysis of the Power Budget and Stability of High-Pressure Nonequilibrium Air Plasmas
| author4 = S.A. Zhdanok
| booktitle=Proceedings of 31st AIAA Plasmadynamics and Lasers Conference, June 19&ndash;22,2000
| title = Analysis of the Power Budget and Stability of High-Pressure Nonequilibrium Air Plasmas
| date=2000
|book-title booktitle= Proceedings of 31st AIAA Plasmadynamics and Lasers Conference, June 19&ndash;22,2000
| pages=Paper 00–2418
| date = 2000
| url=http://rclsgi.eng.ohio-state.edu/~adamovic/netl/PowerBudgtHighPlasma.pdf
| pages = Paper 00–2418
}}</ref> It is theoretically possible to reduce RCS in this way, but it may be very difficult to do so in practice.
|url url= http://rclsgi.eng.ohio-state.edu/~adamovic/netl/PowerBudgtHighPlasma.pdf
|url-status = dead
|archive-url = https://web.archive.org/web/20060910192951/http://rclsgi.eng.ohio-state.edu/~adamovic/netl/PowerBudgtHighPlasma.pdf
|archive-date = 2006-09-10
}}</ref> It is theoretically possible to reduce RCS in this way, but it may be very difficult to do so in practice. Some Russian missiles e.g. the [[3M22 Zircon]] (SS-N-33) and [[Kh-47M2 Kinzhal]] missiles have been reported to make use of plasma stealth.
 
==First claims==
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}}</ref>
 
During Project OXCART, the operation of the [[Lockheed A-12]] reconnaissance aircraft, the CIA funded an attempt to reduce the RCS of the A-12's [[inlet cone]]s. Known as Project KEMPSTER, this used an electron beam generator to create a cloud of ionization in front of each inlet. The system was flight tested but was never deployed on operational A-12s or [[SR-71 Blackbird|SR-71s]].<ref>[http://www.blackbirds.net/sr71/oxcart/successortou2.html ''The U-2's Intended Successor: Project Oxcart 1956-1968'', approved for release by the CIA in October 1994. Retrieved: 26 January 2007].</ref> The A-12 also had the capability to use a [[cesium]]-based fuel additive called "A-50" to ionize the exhaust gases, thus blocking radar waves from reflecting off the aft quadrant and engine exhaust pipes. Cesium was used because it was easily ionized by the hot exhaust gases. Radar physicist Ed Lovick Jr. claimed this additive saved the A-12 program.<ref>{{cite web|url=https://www.thedrive.com/the-war-zone/29787/the-sr-71-blackbirds-predecessor-created-plasma-stealth-by-burning-cesium-laced-fuel|author=Joseph Trevithick and Tyler Rogoway|date=September 12, 2019|title=The SR-71 Blackbird's Predecessor Created "Plasma Stealth" By Burning Cesium-Laced Fuel|publisher=The Drive}}</ref>
 
In 1992, Hughes Research Laboratory conducted a research project to study electromagnetic wave propagation in unmagnetized plasma. A series of high voltage spark gaps were used to generate UV radiation, which creates plasma via photoionization in a waveguide. Plasma filled missile radomeradomes were tested in an anechoic chamber for attenuation of reflection.<ref>{{cite book|last1=Gregoire|first1=D. J.|last2=Santoro|first2=J.|last3=Schumacher|first3=R. W.|title=Electromagnetic-Wave Propagation in Unmagnetized Plasmas.|date=1992|publisher=Air Force Office of Scientific Research|url=https://www.ntis.gov/Search/Home/titleDetail/?abbr=ADA250710|access-date=2015-04-14|archive-url=https://web.archive.org/web/20160304000440/https://www.ntis.gov/Search/Home/titleDetail/?abbr=ADA250710|archive-date=2016-03-04|url-status=dead}}</ref> At about the same time, R. J. Vidmar studystudied the use of atmospheric pressure plasma as electromagnetic reflectors and absorbers.<ref>{{cite journal|last1=Vidmar|first1=Robert J.|title=On the Use of Atmospheric Pressure Plasmas as Electromagnetic Reflectors and Absorbers|journal=IEEE Trans.Transactions on Plasma Science|date=August 1990|volume=18|issue=4|pages=733–741|urlbibcode=http://ieeexplore1990ITPS.ieee.org/xpl/login.jsp?tp18..733V|doi=&arnumber=57528&url=http%3A%2F%2Fieeexplore10.ieee1109/27.org%2Fxpls%2Fabs_all.jsp%3Farnumber%3D5752857528}}</ref> Other investigators also studied the case of a non-uniform magnetized plasma slab.<ref>Laroussi, M. and Roth, J. R “Numerical calculation of the reflection, absorption, and transmission of microwaves by a non-uniform plasma slab”, IEEE Trans. Plasma Sci. 21, 366 (1993)</ref>
 
Despite the apparent technical difficulty of designing a plasma stealth device for combat aircraft, there are claims that a system was offered for export by [[Russia]] in 1999. In January 1999, the Russian [[ITAR-TASS]] news agency published an interview with Doctor [[Anatoliy Koroteyev]], the director of the Keldysh Research Center (FKA Scientific Research Institute for Thermal Processes), who talked about the plasma stealth device developed by his organization. The claim was particularly interesting in light of the solid scientific reputation of Dr. Koroteyev and the Institute for Thermal Processes,{{Citation needed|date=April 2010}} which is one of the top scientific research organizations in the world in the field of fundamental physics.<ref>Nikolay Novichkov.''Russian scientists created revolutionary technologies for reducing radar visibility of aircraft''. "ITAR-TASS", January 20, 1999.</ref>
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{{Main|Plasma (physics)}}
 
A plasma is a ''[[Plasma (physics)#PotentialsPlasma potential|quasineutral]]'' (total [[electrical charge]] is close to zero) mix of [[ion]]s ([[atom]]s which have been ionized, and therefore possess a net positive charge), [[electron]]s, and neutral particles (un-ionized atoms or molecules). Most plasmas are only partially ionized, in fact, the ionization degree of common plasma devices like fluorescent lamp is fairly low ( less than 1%). Almost all the matter in the universe is very low density plasma: solids, liquids and gases are uncommon away from planetary bodies. Plasmas have many technological applications, from fluorescent lighting to plasma processing for semiconductor manufacture.
 
Plasmas can interact strongly with electromagnetic radiation: this is why plasmas might plausibly be used to modify an object's radar signature. Interaction between plasma and electromagnetic radiation is strongly dependent on the physical properties and parameters of the plasma, most notably the electron temperature and plasma density.
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:<math>\omega_{pe} = (4\pi n_ee^2/m_e)^{1/2} = 5.64 \times 10^4 n_e^{1/2} \mbox{rad/s} = 9000 \times n_e^{1/2} \mbox{Hz} </math>
 
Plasmas can have a wide range of values in both temperature and density; plasma temperatures range from close to absolute zero and to well beyond 10<sup>9</sup> [[kelvin]]s (for comparison, tungsten melts at 3700 kelvins), and plasma may contain less than one particle per cubic metre, or be denser than lead. Electron temperature is usually expressed as electronvolt (eV), and 1 eV is equivalent to 11,604 K. Common plasmas temperature and density in fluorescent light tubes and semiconductor manufacturing processes are around several eV and 10<sup>9-12</sup>per cm<sup>3</sup>. For a wide range of parameters and frequencies, plasma is electrically conductive, and its response to low-frequency electromagnetic waves is similar to that of a metal: a plasma simply reflects incident low-frequency radiation. Low-frequency means it is lower than the characteristic electron plasma frequency.<ref>[[Plasma parameters|plasma frequency]]</ref>. The use of plasmas to control the reflected electromagnetic radiation from an object (Plasma stealth) is feasible at suitable frequency where the conductivity of the plasma allows it to interact strongly with the incoming radio wave, and the wave can either be absorbed and converted into thermal energy, or reflected, or transmitted depending on the relationship between the radio wave frequency and the characteristic plasma frequency. If the frequency of the radio wave is lower than the plasma frequency, it is reflected. if it is higher, it transmitis transmitted. If these two are equal, then resonance occurs. There areis also another mechanism where reflection can be reduced. If the electromagnetic wave passes through the plasma, and is reflected by the metal, and the reflected wave and incoming wave are roughly equal in power, then they may form two phasors. When these two phasors are of opposite phase they can cancel each other out. In order to obtain substantial attenuation of radar signal, the plasma slab needs adequate thickness and density.<ref name=Chung1 />
 
Plasmas support a wide range of waves, but for unmagnetised plasmas, the most relevant are the [[Langmuir wave]]s, corresponding to a dynamic compression of the electrons. For magnetised plasmas, many different wave modes can be excited which might interact with radiation at radar frequencies.
 
== Plasmas on aerodynamic surfaces ==
 
Plasma layers around aircraft have been considered for purposes other than stealth. There are many research papers on the use of plasma to reduce aerodynamic [[Drag (physics)|drag]]. In particular, [[electrohydrodynamic]] coupling can be used to accelerate air flow near an aerodynamic surface. One paper<ref name="drag">{{cite journal
| author=J. Reece Roth
| title=Aerodynamic flow acceleration using paraelectric and peristaltic electrohydrodynamic „(EHD) effects of a One Atmosphere Uniform Glow Discharge Plasma „(OAUGDP)''''
| journal=Physics of Plasmas
| date=2003
| volume=10
| pages=2127&ndash;2135
|bibcode = 2003PhPl...10.2127K |doi = 10.1063/1.1563260
| last2=Balkey
| first2=M. M.
| last3=Keiter
| first3=P. A.
| last4=Scime
| first4=E. E.
| last5=Keesee
| first5=A. M.
| last6=Sun
| first6=X.
| last7=Hardin
| first7=R.
| last8=Compton
| first8=C.
| last9=Boivin
| first9=R. F.
| displayauthors=8
| issue=5 }}{{Failed verification|date=September 2014|reason=bibcode and doi do not point to the article named}}</ref> considers the use of a plasma panel for boundary layer control on a wing in a low-speed [[wind tunnel]]. This demonstrates that it is possible to produce a plasma on the skin of an aircraft. Radioactive Xenon [[nuclear poison]] or Polonium isotopes when successfully suspended in generated plasma layers or doped into vehicle hulls, may be utilized in order for a reduction in radar cross-section by generating a plasma layer on the surface.<ref name=Isotope>{{cite web|last1=August|first1=Henry|title=ENERGY ABSORPTION BY A RADIOISOTOPE PRODUCED PLASMA|url=http://patft.uspto.gov/netacgi/nph-Parser?Sect1=PTO2&Sect2=HITOFF&p=1&u=%2Fnetahtml%2FPTO%2Fsearch-bool.html&r=12&f=G&l=50&co1=AND&d=PALL&s1=3713157&OS=3713157&RS=3713157|website=USPTO 3,713,157|accessdate=January 23, 1973}}</ref> If tunable this could shield against HMP/EMP and HERF weaponry or act as optical radiation pressure actuators.
 
Boeing filed a series of patents related to the concept of plasma stealth. In US 7,744,039 B2, Jun. 2010, a system to control air flow with electrical pulses is described. In US 7,988,101 B2, Aug. 2011, a plasma generating device is used to create a plasma flow on the trailing edge, which can change its RCS. In US 8,016,246 B2 Sep. 2011, a plasma actuator system is used to camouflage weapon bay on a fighter when it is open. In US 8,016,247 B2, the plasma actuator system is described in detail, which is basically a dielectric barrier discharge (DBD) device. In US 8,157,528 B1 Apr. 2012, a plasma actuating cascade array for use on rotor blade is described. In US 8,220,753 B2 Jul. 2012, a system for controlling airflow on wing surface with pulsed discharge is described.
 
== Absorption of EM radiation ==
 
When [[Electromagnetic radiation|electromagnetic]] waves, such as radar signals, propagate into a conductive plasma, ions and electrons are displaced as a result of the time varying electric and magnetic fields. The wave field gives energy to the particles. The particles generally return some fraction of the energy they have gained to the wave, but some energy may be permanently absorbed as heat by processes like scattering or resonant acceleration, or transferred into other wave types by [[mode conversion]] or nonlinear effects. A plasma can, at least in principle, absorb all the energy in an incoming wave, and this is the key to plasma stealth. However, plasma stealth implies a substantial reduction of an aircraft's [[Radar cross-section|RCS]], making it more difficult (but not necessarily impossible) to detect. The mere fact of detection of an aircraft by a radar does not guarantee an accurate targeting solution needed to intercept the aircraft or to engage it with missiles. A reduction in RCS also results in a proportional reduction in detection range, allowing an aircraft to get closer to the radar before being detected.
 
The central issue here is frequency of the incoming signal. A plasma will simply reflect radio waves below a certain frequency (characteristic electron plasma frequency). This is the basic principle of short wave radios and long-range communications, because low-frequency radio signals bounce between the Earth and the ionosphere and may therefore travel long distances. Early-warning over-the-horizon radars utilize such low-frequency radio waves (typically lower than 50&nbsp;MHz). Most military airborne and air defense radars, however, operate in VHF, UHF, and microwave band, which have frequencies higher than the characteristic plasma frequency of ionosphere, therefore microwave can penetrate the ionosphere and communication between the ground and communication satellites demonstrates is possible. (''Some'' frequencies can penetrate the ionosphere).
 
Plasma surrounding an aircraft might be able to absorb incoming radiation, and therefore reduces signal reflection from the metal parts of the aircraft: the aircraft would then be effectively invisible to radar at long range due to weak signals received.<ref name=Chung1>{{cite book|author1=Shen Shou Max Chung|editor1-last=Wang|editor1-first=Wen-Qin|title=Radar Systems: Technology, Principles and Applications|date=2013|publisher=NOVA Publishers|location=Hauppauge, NY|isbn=978-1-62417-884-9|pages=1–44|edition=1|chapter-url=https://www.novapublishers.com/catalog/product_info.php?products_id=42399|chapter=Chapter 1: Manipulation of Radar Cross Sections with Plasma|doi=10.13140/2.1.4674.4327}}</ref> A plasma might also be used to modify the reflected waves to confuse the opponent's radar system: for example, frequency-shifting the reflected radiation would frustrate Doppler filtering and might make the reflected radiation more difficult to distinguish from noise.
 
Control of plasma properties like density and temperature is important for a functioning plasma stealth device, and it may be necessary to dynamically adjust the plasma density, temperature, or combinations, or the magnetic field, in order to effectively defeat different types of radar systems. The great advantage Plasma Stealth possesses over traditional RFradio Stealthfrequency stealth techniques like shape morphing into [[LOlow-observability geometry]] and use of [[radar-absorbent material]]s is that plasma is tunable and wideband. When faced with frequency hopping radar, it is possible, at least in principle, to change the plasma temperature and density to deal with the situation. The greatest challenge is to generate a large area or volume of plasma with good energy efficiency.
 
Plasma stealth technology also faces various technical problems. For example, the plasma itself emits EM radiation, fortunatelyalthough thisit is usually weak and noise-like in spectrum. Also, it takes some time for plasma to be re-absorbed by the atmosphere and a trail of ionized air would be created behind the moving aircraft, but at present there is no method to detect this kind of plasma trail at long distance. Thirdly, plasmas (like glow discharges or fluorescent lights) tend to emit a visible glow: this is not compatible with overall low observability concept. However, present optical detection devices like FLIR has a shorter range than radar, so Plasma Stealth still has an operational range space. Last but not the least, it is extremely difficult to produce a radar-absorbent plasma around an entire aircraft traveling at high speed, the electrical power needed is tremedoustremendous. However, a substantial reduction of an aircraft's RCS may be still be achieved by generating radar-absorbent plasma around the most reflective surfaces of the aircraft, such as the turbojet engine fan blades, engine air intakes, vertical stabilizers, and airborne radar antenna.
 
|bibcodeThere =have 2009ITPSbeen several computational studies on plasma-based radar cross section reduction technique using three-dimensional finite-difference time-domain simulations...37.2116C }}</ref> Chung studied the radar cross change of a metal cone when it is covered with plasma, a phenomenon that occurs during reentry into the atmosphere.<ref name=Chung2>{{cite journal|last1=Chung|first1=Shen Shou Max|title=FDTD Simulations on Radar Cross Sections of Metal Cone and Plasma Covered Metal Cone|journal=Vacuum|date=Feb 8, 2012|volume=86|issue=7|pages=970–984|doi=10.1016/j.vacuum.2011.08.016|url=http://www.sciencedirect.com/science/article/pii/S0042207X11003411|publisher=ELSEVIER|bibcode = 2012Vacuu..86..970M }}</ref> Chung simulated the radar cross section of a generic satellite, and also the radar cross section when it is covered with artificially generated plasma cones.<ref name=Chung3>{{cite journal|last1=Chung|first1=Shen Shou Max|title=Simulation on Change of Generic Satellite Radar Cross Section via Artificially Created Plasma Sprays|journal=Plasma SourceSources Science and Technology|date=Mar 30, 2016|volume=25|issue=3|pages=035004|doi=10.1088/0963-0252/25/3/035004|bibcode = 2016PSST...25c5004C |s2cid=101719978 }}</ref>
There have been several computational studies on plasma-based radar cross section reduction technique using three-dimensional FDTD simulations. Chaudhury et al. studied the electromagnetic wave attenuation of an Epstein profile plasma using FDTD.<ref name="3drcs">{{cite journal
| doi=10.1109/TPS.2009.2032331
| author=Bhaskar Chaudhury
| author2=Shashank Chaturvedi
| last-author-amp=yes
| title=Study and Optimization of Plasma-Based Radar Cross Section Reduction Using Three-Dimensional Computations
| journal=Ieee Transactions on Plasma Science
| date=2009
| volume=37
| issue=11
| pages=2116&ndash;2127
| url=http://ieeexplore.ieee.org/xpl/freeabs_all.jsp?isnumber=5313577&arnumber=5306109&count=24&index=1
|bibcode = 2009ITPS...37.2116C }}</ref> Chung studied the radar cross change of a metal cone when it is covered with plasma, a phenomenon that occurs during reentry into the atmosphere.<ref name=Chung2>{{cite journal|last1=Chung|first1=Shen Shou Max|title=FDTD Simulations on Radar Cross Sections of Metal Cone and Plasma Covered Metal Cone|journal=Vacuum|date=Feb 8, 2012|volume=86|issue=7|pages=970–984|doi=10.1016/j.vacuum.2011.08.016|url=http://www.sciencedirect.com/science/article/pii/S0042207X11003411|publisher=ELSEVIER|bibcode = 2012Vacuu..86..970M }}</ref> Chung simulated the radar cross section of a generic satellite, and also the radar cross section when it is covered with artificially generated plasma cones.<ref name=Chung3>{{cite journal|last1=Chung|first1=Shen Shou Max|title=Simulation on Change of Generic Satellite Radar Cross Section via Artificially Created Plasma Sprays|journal=Plasma Source Science and Technology|date=Mar 30, 2016|volume=25|pages=035004|doi=10.1088/0963-0252/25/3/035004|bibcode = 2016PSST...25c5004C }}</ref>
 
== Theoretical work with Sputnik ==
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==See also==
* [[Stealth technology]]
*[[List of plasma (physics) articles]]
* [[StealthActive technologycamouflage]]
* [[Multi-spectral camouflage]]
* [[Cloaking device]]
* [[Penetration aid]]
 
==References==
{{Reflist|30em}}
 
[[Category:Radar]]
[[Category:Plasma physicstechnology and applications|stealth]]
[[Category:Stealth technology]]