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Stealth technology also termed low observable technology (LO technology) is a sub-discipline of military tactics and passive electronic countermeasures, which cover a range of techniques used with personnel, aircraft, ships, submarines, missiles and satellites to make them less visible (ideally invisible) to radar, infrared, sonar and other detection methods. It corresponds to military camouflage for these parts of the electromagnetic spectrum (Multi-spectral camouflage).
Development of modern stealth technologies in the United States began in 1958, where earlier attempts in preventing radar tracking of its U-2 spy planes during the Cold War by the Soviet Union had been unsuccessful. Designers turned to develop a particular shape for planes that tended to reduce detection by redirecting electromagnetic waves from radars. Radar-absorbent material was also tested and made to reduce or block radar signals that reflect off from the surface of planes. Such changes to shape and surface composition form stealth technology as currently used on the Northrop Grumman B-2 Spirit "Stealth Bomber".
The concept of stealth is to operate or hide without giving enemy forces any indications as to the presence of friendly forces. This concept was first explored through camouflage by blending into the background visual clutter. As the potency of detection and interception technologies (radar, Infra-red search and track, surface-to-air missiles, etc.) have increased over time, so too has the extent to which the design and operation of military personnel and vehicles have been affected in response. Some military uniforms are treated with chemicals to reduce their infrared signature. A modern "stealth" vehicle is designed from the outset to have a chosen spectral signature. The degree of stealth embodied in a particular design is chosen according to the predicted capabilities of projected threats.
The concept of camouflage is known to predate warfare itself. Hunters have been using vegetation to conceal themselves perhaps as long as people have been hunting. In England, irregular units of gamekeepers in the 17th century were the first to adopt drab colours (common in 16th century Irish units) as a form of camouflage, following examples from the continent.
During World War I, the Germans experimented with the use of Cellon (Cellulose acetate), a transparent covering material, in an attempt to reduce the visibility of military aircraft. Single examples of the Fokker E.III Eindecker fighter monoplane, the Albatros C.I two-seat observation biplane, and the Linke-Hofmann R.I prototype heavy bomber were covered with Cellon. In fact, sunlight glinting from the material made the aircraft even more visible. Cellon was also found to be quickly degraded both by sunlight and in-flight temperature changes so the attempt to make transparent aircraft was not proceeded with.
In 1916, the British modified a small SS class airship for the purpose of night-time reconnaissance over German lines on the Western Front. Fitted with a silenced engine and a black gas bag, the craft was both invisible and inaudible from the ground but several night-time flights over German-held territory produced little useful intelligence and the idea was dropped.
Diffused lighting camouflage, a shipborne form of counter-illumination camouflage, was trialled by the Royal Canadian Navy from 1941 to 1943. The concept was followed up, but for aircraft, by the Americans and the British: in 1945 a Grumman Avenger with Yehudi lights, reached 3,000 yards (2,700 m) from a ship before being sighted. This ability was rendered obsolete by radar.
The U-boat U-480 may have been the first stealth submarine. It featured an anechoic tile rubber coating, one layer of which contained circular air pockets to defeat ASDIC sonar. Radar absorbent rubber/semiconductor composite paints and materials (codenames: "Sumpf", "Schornsteinfeger") were used by the Kriegsmarine on submarines in World War II. Tests showed they were effective in reducing radar signatures at both short (centimetres) and long (1.5 metre) wavelengths.
In 1960, the first stealth technology development program was initiated by USAF, by reducing the radar-cross-section of a Ryan Q-2C Firebee drone. This was achieved through specially designed screens over the air intake, radar-absorbent material on the fuselage and a special radar-absorbing paint.
In 1958, the U.S. Central Intelligence Agency requested funding for a reconnaissance aircraft to replace the existing U-2 spy planes, and Lockheed secured contractual rights to produce it. "Kelly" Johnson and his team at Lockheed's Skunk Works were assigned to produce the A-12 (or OXCART), the first of the previously top secret Blackbird series, which operated at high altitude of 70,000 to 80,000 ft and speed of Mach 3.2 to avoid radar detection. Radar absorbent material was used on U-2 spy planes, and various plane shapes designed to reduce radar detection were developed in earlier prototypes, named A1 to A11. In 1964, an optimal plane shape taking into account compactness was developed for another "Blackbird", the Lockheed SR-71. This aircraft surpassed prior models in both altitude (90,000 ft) and speed (Mach 3.3). The SR-71 included a number of stealthy features, notably its canted vertical stabilizers, the use of composite materials in key locations, and the overall finish in radar absorbing paint.
During the 1970s the U.S. Department of Defense launched project Lockheed Have Blue, with the aim of developing a stealth fighter. There was fierce bidding between Lockheed and Northrop to secure the multibillion-dollar contract. Lockheed incorporated into its bid a text written by the Soviet/Russian physicist Pyotr Ufimtsev from 1962, titled Method of Edge Waves in the Physical Theory of Diffraction, Soviet Radio, Moscow, 1962. In 1971 this book was translated into English with the same title by U.S. Air Force, Foreign Technology Division. The theory played a critical role in the design of American stealth-aircraft F-117 and B-2. Equations outlined in the paper quantified how a plane's shape would affect its detectability by radar, its radar cross-section (RCS). This was applied by Lockheed in computer simulation to design a novel shape they called the "Hopeless Diamond", a wordplay on the Hope Diamond, securing contractual rights to produce the F-117 Nighthawk starting in 1975. In 1977 Lockheed produced two 60% scale models under the Have Blue contract. The Have Blue program was a stealth technology demonstrator that lasted from 1976 to 1979. Also the Northrop Grumman Tacit Blue played a part in the development of composite material and curvilinear surfaces, as well as Low Observables, fly-by-wire, and other stealth technology innovations. The success of Have Blue led the Air Force to create the Senior Trend program which developed the F-117.
Stealth technology (or LO for "low observability") is not a single technology. It is a combination of technologies that attempt to greatly reduce the distances at which a person or vehicle can be detected; in particular radar cross section reductions, but also acoustic, thermal, and other aspects.
Radar cross-section (RCS) reductionsEdit
Almost since the invention of radar, various methods have been tried to minimize detection. Rapid development of radar during World War II led to equally rapid development of numerous counter radar measures during the period; a notable example of this was the use of chaff. Modern methods include Radar jamming and deception.
The term "stealth" in reference to reduced radar signature aircraft became popular during the late eighties when the Lockheed Martin F-117 stealth fighter became widely known. The first large scale (and public) use of the F-117 was during the Gulf War in 1991. However, F-117A stealth fighters were used for the first time in combat during Operation Just Cause, the United States invasion of Panama in 1989. Increased awareness of stealth vehicles and the technologies behind them is prompting the development of means to detect stealth vehicles, such as passive radar arrays and low-frequency radars. Many countries nevertheless continue to develop low-RCS vehicles because they offer advantages in detection range reduction and amplify the effectiveness of on-board systems against active radar homing threats.
The possibility of designing aircraft in such a manner as to reduce their radar cross-section was recognized in the late 1930s, when the first radar tracking systems were employed, and it has been known since at least the 1960s that aircraft shape makes a significant difference in detectability. The Avro Vulcan, a British bomber of the 1960s, had a remarkably small appearance on radar despite its large size, and occasionally disappeared from radar screens entirely. It is now known that it had a fortuitously stealthy shape apart from the vertical element of the tail. Despite being designed before a low radar cross-section (RCS) and other stealth factors were ever a consideration, a Royal Aircraft Establishment technical note of 1957 stated that of all the aircraft so far studied, the Vulcan appeared by far the simplest radar echoing object, due to its shape: only one or two components contributing significantly to the echo at any aspect, compared with three or more on most other types. While writing about radar systems, authors Simon Kingsley and Shaun Quegan singled out the Vulcan's shape as acting to reduce the RCS. In contrast, the Tupolev 95 Russian long-range bomber (NATO reporting name 'Bear') was conspicuous on radar. It is now known that propellers and jet turbine blades produce a bright radar image; the Bear has four pairs of large (5.6 meter diameter) contra-rotating propellers.
Another important factor is internal construction. Some stealth aircraft have skin that is radar transparent or absorbing, behind which are structures termed re-entrant triangles. Radar waves penetrating the skin get trapped in these structures, reflecting off the internal faces and losing energy. This method was first used on the Blackbird series (A-12/YF-12A/Lockheed SR-71 Blackbird).
The most efficient way to reflect radar waves back to the emitting radar is with orthogonal metal plates, forming a corner reflector consisting of either a dihedral (two plates) or a trihedral (three orthogonal plates). This configuration occurs in the tail of a conventional aircraft, where the vertical and horizontal components of the tail are set at right angles. Stealth aircraft such as the F-117 use a different arrangement, tilting the tail surfaces to reduce corner reflections formed between them. A more radical method is to eliminate the tail completely, as in the B-2 Spirit. The B-2's clean, low-drag flying wing configuration not only gives it exceptional range but also reduces its radar profile. The flying wing design most closely resembles a so-called infinite flat plate (as vertical control surfaces dramatically increase RCS), the perfect stealth shape, as it would have no angles to reflect back radar waves.
In addition to altering the tail, stealth design must bury the engines within the wing or fuselage, or in some cases where stealth is applied to an extant aircraft, install baffles in the air intakes, so that the compressor blades are not visible to radar. A stealthy shape must be devoid of complex bumps or protrusions of any kind, meaning that weapons, fuel tanks, and other stores must not be carried externally. Any stealthy vehicle becomes un-stealthy when a door or hatch opens.
Parallel alignment of edges or even surfaces is also often used in stealth designs. The technique involves using a small number of edge orientations in the shape of the structure. For example, on the F-22A Raptor, the leading edges of the wing and the tail planes are set at the same angle. Other smaller structures, such as the air intake bypass doors and the air refueling aperture, also use the same angles. The effect of this is to return a narrow radar signal in a very specific direction away from the radar emitter rather than returning a diffuse signal detectable at many angles. The effect is sometimes called "glitter" after the very brief signal seen when the reflected beam passes across a detector. It can be difficult for the radar operator to distinguish between a glitter event and a digital glitch in the processing system.
Stealth airframes sometimes display distinctive serrations on some exposed edges, such as the engine ports. The YF-23 has such serrations on the exhaust ports. This is another example in the parallel alignment of features, this time on the external airframe.
Similarly, coating the cockpit canopy with a thin film transparent conductor (vapor-deposited gold or indium tin oxide) helps to reduce the aircraft's radar profile, because radar waves would normally enter the cockpit, reflect off objects (the inside of a cockpit has a complex shape, with a pilot helmet alone forming a sizeable return), and possibly return to the radar, but the conductive coating creates a controlled shape that deflects the incoming radar waves away from the radar. The coating is thin enough that it has no adverse effect on pilot vision.
Ships have also adopted similar methods. Though the earlier Arleigh Burke-class destroyer incorporated some signature-reduction features., the Skjold-class corvette was the first coastal defence and the French La Fayette-class frigate the first ocean-going stealth ship to enter service. Other examples are the Taiwanese Tuo Chiang stealth corvette, German Sachsen-class frigates, the Swedish Visby-class corvette, the USS San Antonio amphibious transport dock, and most modern warship designs.
Dielectric composites are more transparent to radar, whereas electrically conductive materials such as metals and carbon fibers reflect electromagnetic energy incident on the material's surface. Composites may also contain ferrites to optimize the dielectric and magnetic properties of a material for its application.
Radar-absorbent material (RAM), often as paints, are used especially on the edges of metal surfaces. While the material and thickness of RAM coatings can vary, the way they work is the same: absorb radiated energy from a ground or air based radar station into the coating and convert it to heat rather than reflect it back. Current technologies include dielectric composites and metal fibers containing ferrite isotopes. Paint comprises depositing pyramid like colonies on the reflecting superficies with the gaps filled with ferrite-based RAM. The pyramidal structure deflects the incident radar energy in the maze of RAM. A commonly used material is known as "Iron Ball Paint‟. Iron ball paint contains microscopic iron spheres that resonate in tune with incoming radio waves and dissipate the majority of their energy as heat, leaving little to bounce back to detectors. FSS are planar periodic structures that behave like filters to electromagnetic energy. The considered frequency selective surfaces are composed of conducting patch elements pasted on the ferrite layer. FSS are used for filtration and microwave absorption.
Radar stealth countermeasures and limitsEdit
Shaping offers far fewer stealth advantages against low-frequency radar. If the radar wavelength is roughly twice the size of the target, a half-wave resonance effect can still generate a significant return. However, low-frequency radar is limited by lack of available frequencies (many are heavily used by other systems), by lack of accuracy of the diffraction-limited systems given their long wavelengths, and by the radar's size, making it difficult to transport. A long-wave radar may detect a target and roughly locate it, but not provide enough information to identify it, target it with weapons, or even to guide a fighter to it. Noise poses another problem, but that can be efficiently addressed using modern computer technology; Chinese "Nantsin" radar and many older Soviet-made long-range radars have been modified by supporting them with modern computers.
Much of the stealth comes in directions different than a direct return. Thus, detection can be better achieved if emitters are separate from receivers. One emitter separate from one receiver is termed bistatic radar; one or more emitters separate from more than one receiver is termed multistatic radar. Proposals exist to use reflections from emitters such as civilian radio transmitters, including cellular telephone radio towers.
Ship's wakes and sprayEdit
Synthetic Aperture sidescan radars can be used to detect the location and heading of ships from their wake patterns. These may be detectable from orbit. When a ship moves through a seaway it throws up a cloud of spray which can be detected by radar.
Anything that disturbs the atmosphere may be detected (Schlieren photography) because of the Schlieren effect caused by that atmospheric disturbance. This type of Measurement and signature intelligence detection falls under the category of Electro-optical MASINT.
Acoustic stealth plays a primary role in submarine stealth as well as for ground vehicles. Submarines use extensive rubber mountings to isolate and avoid mechanical noises that could reveal locations to underwater passive sonar arrays.
Early stealth observation aircraft used slow-turning propellers to avoid being heard by enemy troops below. Stealth aircraft that stay subsonic can avoid being tracked by sonic boom. The presence of supersonic and jet-powered stealth aircraft such as the SR-71 Blackbird indicates that acoustic signature is not always a major driver in aircraft design, as the Blackbird relied more on its extremely high speed and altitude.
One possible technique for reducing helicopter rotor noise is 'modulated blade spacing'. Standard rotor blades are evenly spaced, and produce greater noise at a particular frequency and its harmonics. Using varying degrees of spacing between the blades spreads the noise or acoustic signature of the rotor over a greater range of frequencies.
The simplest technology is visual camouflage; the use of paint or other materials to color and break up the lines of the vehicle or person.
Most stealth aircraft use matte paint and dark colors, and operate only at night. Lately, interest in daylight Stealth (especially by the USAF) has emphasized the use of gray paint in disruptive schemes, and it is assumed that Yehudi lights could be used in the future to hide the airframe (against the background of the sky, including at night, aircraft of any colour appear dark) or as a sort of active camouflage. The original B-2 design had wing tanks for a contrail-inhibiting chemical, alleged by some to be chlorofluorosulfonic acid, but this was replaced in the final design with a contrail sensor that alerts the pilot when he should change altitude and mission planning also considers altitudes where the probability of their formation is minimized.
In space, mirrored surfaces can be employed to reflect views of empty space toward known or suspected observers; this approach is compatible with several radar stealth schemes. Careful control of the orientation of the satellite relative to the observers is essential, and mistakes can lead to detectability enhancement rather than the desired reduction.
An exhaust plume contributes a significant infrared signature. One means to reduce IR signature is to have a non-circular tail pipe (a slit shape) to minimize the exhaust cross sectional area and maximize the mixing of hot exhaust with cool ambient air (see Lockheed F-117 Nighthawk). Often, cool air is deliberately injected into the exhaust flow to boost this process (see Ryan AQM-91 Firefly and Northrop Grumman B-2 Spirit). According to the Stefan–Boltzmann law, this results in less energy (Thermal radiation in infrared spectrum) being released and thus reduces the heat signature. Sometimes, the jet exhaust is vented above the wing surface to shield it from observers below, as in the Lockheed F-117 Nighthawk, and the unstealthy Fairchild Republic A-10 Thunderbolt II. To achieve infrared stealth, the exhaust gas is cooled to the temperatures where the brightest wavelengths it radiates are absorbed by atmospheric carbon dioxide and water vapor, dramatically reducing the infrared visibility of the exhaust plume. Another way to reduce the exhaust temperature is to circulate coolant fluids such as fuel inside the exhaust pipe, where the fuel tanks serve as heat sinks cooled by the flow of air along the wings.
Reducing radio frequency (RF) emissionsEdit
In addition to reducing infrared and acoustic emissions, a stealth vehicle must avoid radiating any other detectable energy, such as from onboard radars, communications systems, or RF leakage from electronics enclosures. The F-117 uses passive infrared and low light level television sensor systems to aim its weapons and the F-22 Raptor has an advanced LPI radar which can illuminate enemy aircraft without triggering a radar warning receiver response.
The size of a target's image on radar is measured by the radar cross section or RCS, often represented by the symbol σ and expressed in square meters. This does not equal geometric area. A perfectly conducting sphere of projected cross sectional area 1 m2 (i.e. a diameter of 1.13 m) will have an RCS of 1 m2. Note that for radar wavelengths much less than the diameter of the sphere, RCS is independent of frequency. Conversely, a square flat plate of area 1 m2 will have an RCS of σ = 4π A2 / λ2 (where A=area, λ=wavelength), or 13,982 m2 at 10 GHz if the radar is perpendicular to the flat surface. At off-normal incident angles, energy is reflected away from the receiver, reducing the RCS. Modern stealth aircraft are said to have an RCS comparable with small birds or large insects, though this varies widely depending on aircraft and radar.
If the RCS was directly related to the target's cross-sectional area, the only way to reduce it would be to make the physical profile smaller. Rather, by reflecting much of the radiation away or by absorbing it, the target achieves a smaller radar cross section.
Stealthy strike aircraft such as the Lockheed F-117 Nighthawk, designed by the famous Skunk Works, are usually used against heavily defended enemy sites such as Command and control centers or surface-to-air missile (SAM) batteries. Enemy radar will cover the airspace around these sites with overlapping coverage, making undetected entry by conventional aircraft nearly impossible. Stealthy aircraft can also be detected, but only at short ranges around the radars; for a stealthy aircraft there are substantial gaps in the radar coverage. Thus a stealthy aircraft flying an appropriate route can remain undetected by radar. Many ground-based radars exploit Doppler filter to improve sensitivity to objects having a radial velocity component with respect to the radar. Mission planners use their knowledge of enemy radar locations and the RCS pattern of the aircraft to design a flight path that minimizes radial speed while presenting the lowest-RCS aspects of the aircraft to the threat radar. To be able to fly these "safe" routes, it is necessary to understand an enemy's radar coverage (see electronic intelligence). Airborne or mobile radar systems such as AWACS can complicate tactical strategy for stealth operation.
After the invention of metasurfaces, the conventional techniques of reducing RCS have significantly been improved. As mentioned earlier, the primary objective in purpose shaping is to redirect scattered waves away from the backscattered direction (or the source). However, it compromises the performance in terms of aerodynamics. One feasible solution, which has extensively been explored in recent time, is to utilize metasurfaces which can redirect scattered waves without altering the geometry of the target. Such metasurfaces can primarily be classified in two categories: (i) Checkerboard metasurfaces, (ii) Gradient index metasurfaces. Similarly, Negative index metamaterials are artificial structures for which refractive index has a negative value for some frequency range, such as in microwave, infrared, or possibly optical. These offer another way to reduce detectability, and may provide electromagnetic near-invisibility in designed wavelengths.
Plasma stealth is a phenomenon proposed to use ionized gas (plasma) to reduce RCS of vehicles. Interactions between electromagnetic radiation and ionized gas have been studied extensively for many purposes, including concealing vehicles from radar. Various methods might form a layer or cloud of plasma around a vehicle to deflect or absorb radar, from simpler electrostatic to RF more complex laser discharges, but these may be difficult in practice.
Several technology research and development efforts exist to integrate the functions of aircraft flight control systems such as ailerons, elevators, elevons, flaps, and flaperons into wings to perform the aerodynamic purpose with the advantages of lower RCS for stealth via simpler geometries and lower complexity (mechanically simpler, fewer or no moving parts or surfaces, less maintenance), and lower mass, cost (up to 50% less), drag (up to 15% less during use) and, inertia (for faster, stronger control response to change vehicle orientation to reduce detection). Two promising approaches are flexible wings, and fluidics.
In flexible wings, much or all of a wing surface can change shape in flight to deflect air flow. Adaptive compliant wings are a military and commercial effort. The X-53 Active Aeroelastic Wing was a US Air Force, Boeing, and NASA effort.
In fluidics, fluid injection is being researched for use in aircraft to control direction, in two ways: circulation control and thrust vectoring. In both, larger more complex mechanical parts are replaced by smaller, simpler fluidic systems, in which larger forces in fluids are diverted by smaller jets or flows of fluid intermittently, to change the direction of vehicles.
In thrust vectoring, in jet engine nozzles, swiveling parts are replaced by slots which inject fluid flows into jets to divert thrust. Tests show that air forced into a jet engine exhaust stream can deflect thrust up to 15 degrees. The U.S. FAA has conducted a study about civilizing 3D military thrust vectoring to help jetliners avoid crashes. According to this study, 65% of all air crashes can be prevented by deploying thrust vectoring means.
List of stealth aircraftEdit
List of stealth shipsEdit
- Rao G.A.; Mahulikar S.P. (2002). "Integrated review of stealth technology and its role in airpower". Aeronautical Journal. 106 (1066): 629–641.
- Mahulikar S.P.; Sonawane H.R.; Rao G.A. (2007). "Infrared signature studies of aerospace vehicles". Progress in Aerospace Sciences. 43 (7–8): 218–245. Bibcode:2007PrAeS..43..218M. doi:10.1016/j.paerosci.2007.06.002.
- Richelson, J.T. (10 September 2001). "Science, Technology and the CIA". The National Security Archive. The George Washington University. Retrieved 6 October 2009.
- Merlin, P.W. "Design and Development of the Blackbird: Challenges and Lessons Learned" American Institute of Aeronautics and Astronautics Archived 2013-10-18 at the Wayback Machine. 47th AIAA Aerospace Sciences Meeting Including The New Horizons Forum and Aerospace Exposition 5–8 January 2009, Orlando, Florida. Accessed 2009-10-06.
- Cadirci, S. "RF Stealth (or Low Observable) and Counter- RF Stealth Technologies: Implications of Counter- RF Stealth Solutions for Turkish Air Force Archived 2011-07-20 at the Wayback Machine.." Naval Postgraduate School, Monterey California, Ph.D. Thesis. March 2009. Accessed 6 October 2009.
- Yue, T. (30 November 2001). "Detection of the B-2 Stealth Bomber and a Brief History on "Stealth"". The Tech – Online Edition. Massachusetts Institute of Technology. Retrieved 5 October 2009.
- Haddow, G.W.; Peter M. Grosz (1988). The German Giants – The German R-Planes 1914–1918 (3rd ed.). London: Putnam. ISBN 0-85177-812-7.
- Abbott, Patrick (1989). The British Airship at War, 1914–1918. Terence Dalton. pp. 31–33. ISBN 0861380738.
- German U-Boat: Anti Sonar Coating. Retrieved 18 September 2012.
- Hepcke, Gerhard (2007). "The Radar War, 1930–1945" (PDF). English translation by Hannah Liebmann. Radar World: 45. Retrieved 19 September 2012.
- "1960s AQM-34 Ryan Firebee (USA)". PBS. Retrieved 14 January 2015.
- Poteat, Gene (1998). "Stealth, Countermeasures, and ELINT, 1960–1975" (PDF). Studies in Intelligence. 48 (1): 51–59.
- "Lockheed SR-71 Blackbird."
- National Air Intelligence Center, Wright-Patterson AFB, OH, 1971. Technical Report AD 733203, Defense Technical Information Center of USA, Cameron Station, Alexandria, VA, 22304-6145, USA
- Browne, M.W. "Two rival designers led the way to stealthy warplanes", New York Times, Sci. Times Sec., May 14, 1991.
- Browne, M.W. "Lockheed credits Soviet theory in design of F-117", Aviation Week Space Technology p. 27, December 1991.
- Rich, Ben and L. Janos, Skunk Works, Little Brown, Boston, 1994.
- Knott, E.F; Shaeffer, J.F.; Tuley, M.T. (2004). Radar cross section – Second Edition. Raleigh, North Carolina: SciTech Publishing. pp. 209–214. ISBN 1-891121-25-1. Retrieved 7 October 2009.
- F-117A Senior Trend
- "Senior Trend". Vectorsite.net, 1 April 2008.
- Crocker, H. W. III (2006). Don't Tread on Me. New York: Crown Forum. p. 382. ISBN 978-1-4000-5363-6.
- Sweetman, Bill. "The Bomber that radar cannot see." New Scientist, 4 March 1982.
- Dawson 1957, p. 3.
- Seddon and Goldsmith 1999, p. 343.
- Writing for the American Institute of Aeronautics and Astronautics, J. Seddon and E. L. Goldsmith noted that "Due to its all-wing shape, small vertical fin, and buried engines, at some angles [The Avro Vulcan] was nearly invisible to radar".
- Kingsley and Quegan 1999, p. 293.
- Croddy and Wirtz 2005, pp. 341–342.
- Siuru 1993, pp. 114–115.
- "B-2: The Spirit of Innovation" (PDF). Northrop Grumman Corporation. Retrieved 2015-02-04.
- "DDG-51 Arleigh Burke-class". FAS website. Federation of American Scientists. Archived from the original on 24 December 2013. Retrieved 2 February 2011.
- Benson, Robert (November 1998). "The Arleigh Burke: Linchpin of the Navy". Asia-Pacific Defense Forum. Federation of American Scientists. Retrieved 2 February 2011.
- Maj. Gen. Carlsons briefing on Stealth Fighters, Tuesday, April 20, 1999
- MIT's "The Tech – online edition" article Detection of the B-2 Stealth Bomber and a Brief History on "Stealth" by Tao Yue published November 30, 2001 in (Volume 121, Issue 63)
- Global Opposition Movement Challenges JSF
- The Naval Institute guide to world naval weapon systems By Norman Friedman, Introduction page x
- "Stealth Helicopter: MH-X Advanced Special Operations Helicopter". GlobalSecurity.org. Retrieved 28 April 2012.
- Edwards, Bryan (May 2002). "Psychoacoustic Testing of Modulated Blade Spacing for Main Rotors – NASA/CR-2002-211651". NASA. p. 1.2. CiteSeerX .
- Bush,, Vannevar; Conant, James; et al. (1946). "Camouflage of Sea-Search Aircraft" (PDF). Visibility Studies and Some Applications in the Field of Camouflage. Office of Scientific Research and Development, National Defence Research Committee. pp. 225–240. Retrieved February 12, 2013.
- Aeronautics.ru Archived 2004-01-14 at the Wayback Machine. (Dead link)
- Air and Space mag: Why contrails hang around.
-  Optical Warfare – The New Frontier
- GAO-10-669R Warfighter Support
- 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
- A. Y. Modi; C. A. Balanis; C. R. Birtcher; H. Shaman, "Novel Design of Ultra-Broadband Radar Cross Section Reduction Surfaces using Artificial Magnetic Conductors," in IEEE Transactions on Antennas and Propagation, vol.PP, no.99, pp.1-1. doi: 10.1109/TAP.2017.2734069
- Appl. Phys. Lett. 104, 221110 (2014). doi: 10.1063/1.4881935
- Shelby, R. A.; Smith D.R; Shultz S. (2001). "Experimental Verification of a Negative Index of Refraction". Science. 292 (5514): 77–79. Bibcode:2001Sci...292...77S. doi:10.1126/science.1058847. PMID 11292865.
- I.V. Adamovich; J. W. Rich; A.P. Chernukho; S.A. Zhdanok (2000). "Analysis of the Power Budget and Stability of High-Pressure Nonequilibrium Air Plasmas" (PDF). Proceedings of 31st AIAA Plasmadynamics and Lasers Conference, June 19–22, 2000. pp. Paper 00–2418. Archived from the original (PDF) on 2006-09-10.
- Scott, William B. (27 November 2006), "Morphing Wings", Aviation Week & Space Technology
- "FlexSys Inc.: Aerospace". Archived from the original on 16 June 2011. Retrieved 26 April 2011.
- Kota, Sridhar; Osborn, Russell; Ervin, Gregory; Maric, Dragan; Flick, Peter; Paul, Donald. "Mission Adaptive Compliant Wing – Design, Fabrication and Flight Test" (PDF). Ann Arbor, MI; Dayton, OH, U.S.A.: FlexSys Inc., Air Force Research Laboratory. Archived from the original (PDF) on 22 March 2012. Retrieved 26 April 2011.
- P John (2010). "The flapless air vehicle integrated industrial research (FLAVIIR) programme in aeronautical engineering". Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering. London: Mechanical Engineering Publications. 224 (4): 355–363. doi:10.1243/09544100JAERO580. ISSN 0954-4100. Archived from the original on 2018-06-23.
- "Showcase UAV Demonstrates Flapless Flight". BAE Systems. 2010. Retrieved 2010-12-22.
- "Demon UAV jets into history by flying without flaps". Metro.co.uk. London: Associated Newspapers Limited. 28 September 2010.
- P. J. Yagle; D. N. Miller; K. B. Ginn; J. W. Hamstra (2001). "Demonstration of Fluidic Throat Skewing for Thrust Vectoring in Structurally Fixed Nozzles". Journal of Engineering for Gas Turbines and Power. 123 (3): 502–508. doi:10.1115/1.1361109.
- "Multiaxis Thrust Vectoring Flight Control Vs Catastrophic Failure Prevention", Reports to U.S. Dept. of Transportation/FAA, Technical Center, ACD-210, FAA X88/0/6FA/921000/4104/T1706D, FAA Res. Benjamin Gal-Or, Grant-Award No: 94-G-24, CFDA, No. 20.108, Dec. 26, 1994
- "Vectored Propulsion, Supermanoeuvreability, and Robot Aircraft", by Benjamin Gal-Or, Springer Verlag, 1990, ISBN 0-387-97161-0, 3-540-97161-0.
34. "Multiaxis Thrust Vectoring Flight Control Vs Catastrophic Failure Prevention", Reports to U.S. Dept. of Transportation/FAA, Technical Center, ACD-210, FAA X88/0/6FA/921000/4104/T1706D, FAA Res. Benjamin Gal-Or, Grant-Award No: 94-G-24, CFDA, No. 20.108, Dec. 26, 1994.
- Dawson, T.W.G., G.F. Kitchen and G.B. Glider. Measurements of the Radar Echoing Area of the Vulcan by the Optical Simulation Method. Farnborough, Hants, UK: Royal Aircraft Establishment, September 1957 National Archive Catalogue file, AVIA 6/20895
- Ufimtsev, Pyotr Ya., "Method of edge waves in the physical theory of diffraction," Moscow, Russia: Izd-vo. Sov. Radio [Soviet Radio Publishing], 1962, pages 1–243.
- Doucet, Arnaud; Freitas, Nando de; Gordon, Neil (2001) . Sequential Monte Carlo Methods in Practice. Statistics for Engineering and Information Science (1st ed.). Berlin: Springer-Verlag. ISBN 978-0-387-95146-1. Retrieved 2009-03-11.
- Analogues of Stealth – Northrop Grumman
- Countering stealth
- How "stealth" is achieved on F-117A
- United States Patent No.6,297,762. October 2, 2001. Electronic countermeasures system (Apparatus for detecting the difference in phase between received signals at two spaced antennas and for then retransmitting equal amplitude antiphase signals from the two spaced antennas is disclosed.)
- "Multiaxis Thrust Vectoring Flight Control Vs Catastrophic Failure Prevention", Reports to U.S. Dept. of Transportation/FAA, Technical Center, ACD-210, FAA X88/0/6FA/921000/4104/T1706D, FAA Res. Benjamin Gal-Or, Grant-Award No: 94-G-24, CFDA, No. 20.108, Dec. 26, 1994; "Vectored Propulsion, Supermanoeuvreability, and Robot Aircraft", by Benjamin Gal-Or, Springer Verlag, 1990, ISBN 0-387-97161-0, 3-540-97161-0.
- Suhler, Paul A. From Rainbow to Gusto: Stealth and the Design of the Lockheed Blackbird, American Institute of Aeronautics and Astronautics, 2009. ISBN 1-60086-712-X.