A Short Report
Presented to Mr.
Clyde Smith
Master in
Aeronautical Science
Embry Riddle
Aeronautical University
The principle of Radar Cross Section (RCS) reduction
When
radars were first used, radar engineers thought that the range an aircraft
could detect a target was only related to the target’s physical size. Soon they
realized that this was wrong. They found out that the range was related to the
energy reflected from a target. So they came up with the concept of the Radar
Cross Section. RCS compares the energy reflected from a target with the energy
reflected from a sphere, with cross-sectional area of one square meter.
A flat surface has an extremely large RCS if it is
normal to the radar beam. As the plate is tilted or canted away from the beam
in one dimension, its RCS decreases sharply: reflectivity is reduced by a
factor of 1,000 at a cant angle of 30 degrees. But if the surface is both
canted and swept back-the RCS reduction can be realized at an 8 degrees angle.
This is how they did manage to built an “invisible” aircraft: by constructing
it entirely out of flat surfaces, canted and rotated away from the arrival
angle of any radar beam.
Denys Overholser, when
asked what makes an aircraft stealth, said: “Shape, shape, shape and
materials”. Overholser, although an
electric engineer, is the man who had the idea of the “flat plane” as a stealth
attribute. It is well known that a stealth aircraft also incorporates other
kind of technologies that augment aircraft’s “invisibility”, like Radar
Absorbent Materials (RAM). But an aircraft with a “wrong design” is impossible
to become stealth, and that is why old designs cannot “upgrade” their stealth
capabilities. The LO are the dominant attributes of an aircraft design, that affect
its configuration, external lines and internal arrangements.
The most important
stealth-driven feature of the F-35 is that it caries a 5,000-pound internal
weapon load. The fuel is also carried in tanks inside the fuselage and the
wings, and this is why the JSF is not a small aircraft. It had to be scaled up
to make room for both. The importance of being stealth in all phases of a
mission (inbound-outbound) forbids carrying disposable external fuel tanks,
something usually done with other fighters.
Another
LO characteristic of the JSF is that it has rounded edges where its flat canted
surfaces meet. This can be easily seen in figures 2-4. This way the radar waves
that hit against these edges are deflected away from their source instead of
reflected back to it. Another thing that can also be seen in figures 2-4 is
that all edges are aligned (see red lines). For example the trailing edges of
the wing are aligned with trailing edges of the horizontal stabilizer and with
upper and lower inlet lips on the opposite side of the airplane. The wing and
tail leading edges are aligned with each other. The idea is that it is better
to add energy to the spikes in the radar signature at right angles to each of
the sharp edges than to add more spikes, even small ones, which increase the
probability of detection.
Related
with this technique is the way the JSF’s apertures are treated in order to
avoid electromagnetic discontinuity and unacceptable RCS spikes. All apertures,
including landing gears, maintenance panels, weapon bay doors, antennas, and
the cockpit opening, are designed to follow the primary alignments. Where this
was structurally difficult, the edges where serrated so that the aperture is
basically square.
An also
very important stealth feature is the JSF’s inlet design. Compressor’s face,
with its rotating blades, is a major RCS contributor. Modern radars not only
can detect a plane because of the blades but also identify the target by using
a technique called Jet Engine Modulation (JEM). As you can see on Figure 1,
engine position and inlet design totally hide the engine from radar view. JSF’s
inlet features a shallow smooth bump on the body side, positioned between upper
and lower inlet lips that slant forward, away form the body (Figure 3). This
creates a pressure rise, and the result is that the boundary layer is gently
diverted to either side.
Engine’s
exhaust is a pain from the LO’s point of view and one of the most difficult
tasks. Pratt and Whitney developed a Low-Observable Axisymmetrical Nozzle (LOAN),
which is incorporated in the JSF USAF and Army versions. The system was
thoroughly tested on an F-16. It derived from the Raptor’s exhaust as a
simplified version without thrust vectoring. The exhaust system is also
“hidden” from many angles of view by the vertical and horizontal stabilizers.
The
cockpit of a conventional aircraft is one of the largest sources of radar
signature. Pilot’s helmet, displays and the seats contribute to this. The best
way to “hide” them from the radar is to block radar’s energy. JSF’s canopy is
made of polycarbonate material. It has a metallic coating and is smoothly
blended into the aircraft shape to minimize reflections.
On the F-35 several special materials are used, including Radar Absorbing Materials (RAM), Radar Absorbing Structure and Infrared (IR) Topcoat. Unlike the F-117, which was totally coated with 2,000 pounds of RAM, these materials are more selectively used on the JSF. Lockheed Martin developed paint-type RAM which is applied around the edges of doors and control surfaces. RAS is used on the body, wing and tail edges. For the application of this paint robots will be used, like the CASPER (Computer Aided Spray Paint Expelling Robot) system used for F-22 and the Have Glass II program used for painting 1,700 F-16s with RAM. Robots are essential because they can reach confined areas, as the inlet ducts, and can work without stepping on the aircraft.
These materials comprise ferromagnetic particles, embedded in a high-dielectric-constant polymer base. The dielectric material slows down the wave and the ferromagnetic particles absorb the energy. These coatings are also designed in a way that the small reflection from the front face of the absorber is cancelled by a residual reflection from the structure beneath it. This is not an easy procedure, and it makes RAM design much more tricky than most people believe.
JSF’s entire airframe is also painted with a camouflage topcoat that suppresses IR.
Radome-Radar
JSF’s uses a band-pass resonant radome and is one of its most complex structural components. The Northrop Grumman APG-81 has what is called Active Electronically Scanned Array (AESA). It comprises a fixed planar structure carrying more than 1,000 “transmit-receive modules”, each of them one tiny solid-state radar. Apart from its state of the art detection capabilities, it also contributes to the RCS reduction since it is tilted slightly upwards, deflecting away any possible reflection to any possible receiver.
An aircraft’s identity can easily be betrayed by its radar’s emissions. AESA though, uses many low-probability of intercept (LPI) techniques. For example, it is possible to reduce peak power adaptively, as the target gets closer. The radar power is decreased rapidly to a point where an intercept receiver cannot detect it. AESA can search simultaneously with multiple beams, many small sectors, reducing probability of detection. It also has the capability to confuse interception systems by varying almost every characteristic of its signal between two consecutive pulses.
Conclusion
While maneuverable enough, the F-35 JSF is not designed to be a champion as a dogfighter. Wing loading, thrust-to-weight ratio, armament layout, and cockpit design point to this fact. JSF is a state-of-the-art stealth aircraft. It incorporates every known LO technology. The most probable way to detect it is by its weapons’ noise of impact. It is designed to be the most lethally invisible aircraft ever made.
Shape, shape, shape …
Figure 2
Figure 3
Figure 4
References
Fielding, John P. (1999). Introduction to Aircraft Design. Cambridge University Press.
Haisty, Brett S. (2000). Lockheed Martin’s Affordable Stealth. Washington Press.
Sweetman, Bill (2001). Lockheed’s Stealth (1st Ed). Minnesota: Zenith Press
Sweetman, Bill (2004). Ultimate Fighter (1st Ed). Minnesota: Zenith Press
Web Sites
F-35 JOINT STRIKE FIGHTER PROGRAM (http://www.jsf.mil/index.htm)
F-35 Joint Strike Fighter, Lockheed Martin (http://www.lockheedmartin.com/wms/findPage.do?dsp=fec&ci=11173&rsbci=11173&fti=0&ti=0&sc=400)
JSF (F35) JOINT STRIKE FIGHTER, INTERNATIONAL, Airforce-technology.com (http://www.airforce-technology.com/projects/jsf/)